subject:(UNMANNED AIR VEHICLES AERONAUTICAL ENGINEERING )

University of Colorado

1. Elston, Jack Steward. Semi-Autonomous Small Unmanned Aircraft Systems for Sampling Tornadic Supercell Thunderstorms.

Degree: PhD, Aerospace Engineering Sciences, 2011, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/25

► This work describes the development of a network-centric unmanned aircraft system (UAS) for in situ sampling of supercell thunderstorms. UAS have been identified as… (more)

▼ This work describes the development of a network-centric unmanned aircraft system (UAS) for in situ sampling of supercell thunderstorms. UAS have been identified as a well-suited platform for meteorological observations given their portability, endurance, and ability to mitigate atmospheric disturbances. They represent a unique tool for performing targeted sampling in regions of a supercell thunderstorm previously unreachable through other methods. Doppler radar can provide unique measurements of the wind field in and around supercell thunderstorms. In order to exploit this capability, a planner was developed that can optimize ingress trajectories for severe storm penetration. The resulting trajectories were examined to determine the feasibility of such a mission, and to optimize ingress in terms of flight time and exposure to precipitation. A network-centric architecture was developed to handle the large amount of distributed data produced during a storm sampling mission. Creation of this architecture was performed through a bottom-up design approach which reflects and enhances the interplay between networked communication and autonomous aircraft operation. The advantages of the approach are demonstrated through several field and hardware-in-the-loop experiments containing different hardware, networking protocols, and objectives. Results are provided from field experiments involving the resulting network-centric architecture. An airmass boundary was sampled in the Collaborative Colorado Nebraska Unmanned Aircraft Experiment (CoCoNUE). Utilizing lessons learned from CoCoNUE, a new concept of operations (CONOPS) and UAS were developed to perform in situ sampling of supercell thunderstorms. Deployment during the Verification of the Origins of Rotation in Tornadoes Experiment 2 (VOR- TEX2) resulted in the first ever sampling of the airmass associated with the rear flank downdraft of a tornadic supercell thunderstorm by a UAS. Hardware-in-the-loop simulation capability was added to the UAS to enable further assessment of the system and CONOPS. The simulation combines a full six degree-of-freedom aircraft dynamic model with wind and precipitation data from simulations of severe convective storms. Interfaces were written to involve as much of the system's field hardware as possible, including the creation of a simulated radar product server. A variety of simulations were conducted to evaluate different aspects of the CONOPS used for the 2010 VORTEX2 field campaign. Advisors/Committee Members: Eric W. Frew, Brian M. Argrow, Adam Houston.

Subjects/Keywords: network; supercell; tornado; UAS; unmanned; VORTEX2; Aeronautical Vehicles; Aerospace Engineering; Meteorology

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APA (6^th Edition):

Elston, J. S. (2011). Semi-Autonomous Small Unmanned Aircraft Systems for Sampling Tornadic Supercell Thunderstorms. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/25

Chicago Manual of Style (16^th Edition):

Elston, Jack Steward. “Semi-Autonomous Small Unmanned Aircraft Systems for Sampling Tornadic Supercell Thunderstorms.” 2011. Doctoral Dissertation, University of Colorado. Accessed January 20, 2020. https://scholar.colorado.edu/asen_gradetds/25.

MLA Handbook (7^th Edition):

Elston, Jack Steward. “Semi-Autonomous Small Unmanned Aircraft Systems for Sampling Tornadic Supercell Thunderstorms.” 2011. Web. 20 Jan 2020.

Vancouver:

Elston JS. Semi-Autonomous Small Unmanned Aircraft Systems for Sampling Tornadic Supercell Thunderstorms. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2020 Jan 20]. Available from: https://scholar.colorado.edu/asen_gradetds/25.

Council of Science Editors:

Elston JS. Semi-Autonomous Small Unmanned Aircraft Systems for Sampling Tornadic Supercell Thunderstorms. [Doctoral Dissertation]. University of Colorado; 2011. Available from: https://scholar.colorado.edu/asen_gradetds/25

ETH Zürich

2. Dmitriev, Vitaly. Application of Compliant Structures for Flight Performance Improvement of Unmanned Aerial Vehicles.

Degree: 2014, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/99847

Subjects/Keywords: INTELLIGENTE MATERIALIEN; SMART MATERIALS; UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA (6^th Edition):

Dmitriev, V. (2014). Application of Compliant Structures for Flight Performance Improvement of Unmanned Aerial Vehicles. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/99847

Chicago Manual of Style (16^th Edition):

Dmitriev, Vitaly. “Application of Compliant Structures for Flight Performance Improvement of Unmanned Aerial Vehicles.” 2014. Doctoral Dissertation, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/99847.

MLA Handbook (7^th Edition):

Dmitriev, Vitaly. “Application of Compliant Structures for Flight Performance Improvement of Unmanned Aerial Vehicles.” 2014. Web. 20 Jan 2020.

Vancouver:

Dmitriev V. Application of Compliant Structures for Flight Performance Improvement of Unmanned Aerial Vehicles. [Internet] [Doctoral dissertation]. ETH Zürich; 2014. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/99847.

Council of Science Editors:

Dmitriev V. Application of Compliant Structures for Flight Performance Improvement of Unmanned Aerial Vehicles. [Doctoral Dissertation]. ETH Zürich; 2014. Available from: http://hdl.handle.net/20.500.11850/99847

Embry-Riddle Aeronautical University

3. Haddad, Nicolas El. Aerodynamic and Structural Design of a Winglet for Enhanced Performance of a Business Jet.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/265

► The preliminary design of a winglet to improve the range and fuel burn of the Falcon 10 business jet is presented. Twelve candidate geometries… (more)

Subjects/Keywords: Aeronautical Vehicles; Aerospace Engineering

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APA (6^th Edition):

Haddad, N. E. (2015). Aerodynamic and Structural Design of a Winglet for Enhanced Performance of a Business Jet. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/265

Chicago Manual of Style (16^th Edition):

Haddad, Nicolas El. “Aerodynamic and Structural Design of a Winglet for Enhanced Performance of a Business Jet.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 20, 2020. https://commons.erau.edu/edt/265.

MLA Handbook (7^th Edition):

Haddad, Nicolas El. “Aerodynamic and Structural Design of a Winglet for Enhanced Performance of a Business Jet.” 2015. Web. 20 Jan 2020.

Vancouver:

Haddad NE. Aerodynamic and Structural Design of a Winglet for Enhanced Performance of a Business Jet. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Jan 20]. Available from: https://commons.erau.edu/edt/265.

Council of Science Editors:

Haddad NE. Aerodynamic and Structural Design of a Winglet for Enhanced Performance of a Business Jet. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/265

Embry-Riddle Aeronautical University

4. Park, Min Soon. Aircraft De-Icing System Using Thermal Conductive Fibers.

Degree: MSin Aerospace Engineering, Graduate Studies, 2015, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/276

► The accumulation of ice on the leading edges of aircraft wing poses complications for flight control as drag is increased with a tendency for… (more)

Subjects/Keywords: Aeronautical Vehicles; Aerospace Engineering

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APA (6^th Edition):

Park, M. S. (2015). Aircraft De-Icing System Using Thermal Conductive Fibers. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/276

Chicago Manual of Style (16^th Edition):

Park, Min Soon. “Aircraft De-Icing System Using Thermal Conductive Fibers.” 2015. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 20, 2020. https://commons.erau.edu/edt/276.

MLA Handbook (7^th Edition):

Park, Min Soon. “Aircraft De-Icing System Using Thermal Conductive Fibers.” 2015. Web. 20 Jan 2020.

Vancouver:

Park MS. Aircraft De-Icing System Using Thermal Conductive Fibers. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2015. [cited 2020 Jan 20]. Available from: https://commons.erau.edu/edt/276.

Council of Science Editors:

Park MS. Aircraft De-Icing System Using Thermal Conductive Fibers. [Masters Thesis]. Embry-Riddle Aeronautical University; 2015. Available from: https://commons.erau.edu/edt/276

Embry-Riddle Aeronautical University

5. Kennedy, Christopher Lloyd. Development of an Exteroceptive Sensor Suite on Unmanned Surface Vessels for Real-Time Classification of Navigational Markers.

Degree: MSin Mechanical Engineering, Mechanical Engineering, 2014, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/167

► This thesis presents the development of an exteroceptive sensor suite for real-time detection and classification of navigational markers on Unmanned Surface Vessels. Three sensors… (more)

Subjects/Keywords: Aeronautical Vehicles; Mechanical Engineering

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APA (6^th Edition):

Kennedy, C. L. (2014). Development of an Exteroceptive Sensor Suite on Unmanned Surface Vessels for Real-Time Classification of Navigational Markers. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/167

Chicago Manual of Style (16^th Edition):

Kennedy, Christopher Lloyd. “Development of an Exteroceptive Sensor Suite on Unmanned Surface Vessels for Real-Time Classification of Navigational Markers.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 20, 2020. https://commons.erau.edu/edt/167.

MLA Handbook (7^th Edition):

Kennedy, Christopher Lloyd. “Development of an Exteroceptive Sensor Suite on Unmanned Surface Vessels for Real-Time Classification of Navigational Markers.” 2014. Web. 20 Jan 2020.

Vancouver:

Kennedy CL. Development of an Exteroceptive Sensor Suite on Unmanned Surface Vessels for Real-Time Classification of Navigational Markers. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Jan 20]. Available from: https://commons.erau.edu/edt/167.

Council of Science Editors:

Kennedy CL. Development of an Exteroceptive Sensor Suite on Unmanned Surface Vessels for Real-Time Classification of Navigational Markers. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/167

Embry-Riddle Aeronautical University

6. Pedroza, Natalie Ramos. Robust and Adaptive Nonlinear Control of Limit Cycle Oscillations in UAVs Using Synthetic Jet Actuators.

Degree: MSin Engineering Physics, Physical Sciences, 2014, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/278

► Limit cycle oscillations (LCO), also known as utter, cause significant challenges in fight control of unmanned aerial vehicles (UAVs), and could potentially lead to… (more)

▼ Limit cycle oscillations (LCO), also known as utter, cause significant challenges in fight control of unmanned aerial vehicles (UAVs), and could potentially lead to structural damage and catastrophic failures. LCO can be described as vibrational motions in the pitching and plunging displacements of an aircraft wing. Even in low Reynolds number (low-Re) fight regimes, LCO can exceed the limiting boundary for safe UAV fight. Further, as practical considerations motivate the design of smaller, lighter weight UAVs, there is a growing need for UAV systems that do not require heavy mechanical actuators (e.g., ailerons). To address this, the use of synthetic jet actuators (SJAs) in UAV fight control systems is becoming popular as a practical alternative to mechanical deflection surfaces. SJAs are promising tools for LCO suppression systems in small UAVs due to their small size, ease of operation, and low cost. Uncertainties inherent in the dynamics of SJAs present significant challenges in SJA-based control design. Specifically, the input-output characteristic of SJAs is nonlinear and contains parametric uncertainty. Further control design challenges exist in situations where multiple actuators lose effectiveness. In the event of loss of effectiveness in multiple actuators, control challenges arise due to the fact that the resulting system contains fewer actuators than degrees of freedom (DOF) to be controlled (i.e., an underactuated system). Still further difficulties exist in control design for dual parallel underatuated systems, where standard backstepping-based control approaches cannot be applied. In this thesis, three nonlinear SJA-based control methods are presented, which are capable of complete (i.e., asymptotic) suppression of LCO in UAV systems containing uncertainty. An adaptive control method is presented first, which is shown to achieve asymptotic regulation of LCO for UAVs in the presence of model uncertainty and unmodelled external disturbances. Motivated by the desire to reduce the computational complexity of the closed-loop system, a structurally simplistic robust (single feedback loop) control design is presented next, which is shown to achieve asymptotic LCO regulation without the need for adaptive parameter estimation. Finally, to address the control challenges encountered in the event of actuator faults, a robust control method is presented, which achieves simultaneous suppression of the pitching and plunging displacements using only a single scalar control input. The control design presented for this underactuated scenario is also proven to completely compensate for the inherent SJA nonlinearity. Rigorous Lyapunov-based stability analyses are provided to prove the theoretical results, and numerical simulation results are provided to complement the theoretical development.

Subjects/Keywords: Aeronautical Vehicles; Engineering Physics

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APA (6^th Edition):

Pedroza, N. R. (2014). Robust and Adaptive Nonlinear Control of Limit Cycle Oscillations in UAVs Using Synthetic Jet Actuators. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/278

Chicago Manual of Style (16^th Edition):

Pedroza, Natalie Ramos. “Robust and Adaptive Nonlinear Control of Limit Cycle Oscillations in UAVs Using Synthetic Jet Actuators.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 20, 2020. https://commons.erau.edu/edt/278.

MLA Handbook (7^th Edition):

Pedroza, Natalie Ramos. “Robust and Adaptive Nonlinear Control of Limit Cycle Oscillations in UAVs Using Synthetic Jet Actuators.” 2014. Web. 20 Jan 2020.

Vancouver:

Pedroza NR. Robust and Adaptive Nonlinear Control of Limit Cycle Oscillations in UAVs Using Synthetic Jet Actuators. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2020 Jan 20]. Available from: https://commons.erau.edu/edt/278.

Council of Science Editors:

Pedroza NR. Robust and Adaptive Nonlinear Control of Limit Cycle Oscillations in UAVs Using Synthetic Jet Actuators. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/278

University of Kentucky

7. Doepke, Edward Brady. DESIGN AND FLIGHT TESTING OF A WARPING WING FOR AUTONOMOUS FLIGHT CONTROL.

Degree: 2012, University of Kentucky

URL: http://uknowledge.uky.edu/me_etds/20

► Inflatable-wing Unmanned Aerial Vehicles (UAVs) have the ability to be packed in a fraction of their deployed volume. This makes them ideal for many deployable… (more)

Subjects/Keywords: Unmanned Aerial Vehicle; UAV; Wing Warping; Wing Morphing; Flight Testing; Aeronautical Vehicles; Other Mechanical Engineering; Structures and Materials

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APA (6^th Edition):

Doepke, E. B. (2012). DESIGN AND FLIGHT TESTING OF A WARPING WING FOR AUTONOMOUS FLIGHT CONTROL. (Masters Thesis). University of Kentucky. Retrieved from http://uknowledge.uky.edu/me_etds/20

Chicago Manual of Style (16^th Edition):

Doepke, Edward Brady. “DESIGN AND FLIGHT TESTING OF A WARPING WING FOR AUTONOMOUS FLIGHT CONTROL.” 2012. Masters Thesis, University of Kentucky. Accessed January 20, 2020. http://uknowledge.uky.edu/me_etds/20.

MLA Handbook (7^th Edition):

Doepke, Edward Brady. “DESIGN AND FLIGHT TESTING OF A WARPING WING FOR AUTONOMOUS FLIGHT CONTROL.” 2012. Web. 20 Jan 2020.

Vancouver:

Doepke EB. DESIGN AND FLIGHT TESTING OF A WARPING WING FOR AUTONOMOUS FLIGHT CONTROL. [Internet] [Masters thesis]. University of Kentucky; 2012. [cited 2020 Jan 20]. Available from: http://uknowledge.uky.edu/me_etds/20.

Council of Science Editors:

Doepke EB. DESIGN AND FLIGHT TESTING OF A WARPING WING FOR AUTONOMOUS FLIGHT CONTROL. [Masters Thesis]. University of Kentucky; 2012. Available from: http://uknowledge.uky.edu/me_etds/20

University of Colorado

8. Laurence, Roger Jean, III. Suas Wind Sensing with Computational Fluid Dynamics and a Distributed Flush Airdata System.

Degree: PhD, Aerospace Engineering Sciences, 2017, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/179

► Small unmanned aircraft systems (sUAS) have proven their effectiveness for measuring both the inertial and aircraft-relative wind. Multiple methods for wind measurement from sUAS… (more)

▼ Small unmanned aircraft systems (sUAS) have proven their effectiveness for measuring both the inertial and aircraft-relative wind. Multiple methods for wind measurement from sUAS exist, but one of the more common instruments is the multi-hole probe (MHP). While the MHP is accurate and simple to use, there are two main drawbacks: 1) the MHP airdata system can cost several times that of the sUAS, and 2) the probe itself is often exposed to damage during routine operations. Flush airdata systems (FADS) are an alternative method of wind sensing, and work with pressure ports mounted flush with the aircraft surface. This removes any external components, thereby mitigating the risk of damage to the airdata system. The work presented details the implementation of a FADS for sUAS. Computational fluid dynamics simulations were used to determine the port locations of the FADS. Airframe locations were sorted based on the total sensitivity over a range of angles of attack and sideslip. Upon completion of hardware installation, the FADS was calibrated in flight using an onboard MHP. A portion of the flight testing was reserved for validation of the FADS. Multi-layer feedforward neural networks are employed to produce estimates of the angle of attack and sideslip, while static and stagnation ports on the fuselage measure airspeed. In the validation portion of flight tests, the FADS exhibited an overall mean error of 0.12 m/s in airspeed, but errors in angle of attack and sideslip were unbiased. Root-mean-square errors were 0.42 m/s, 0.65 ◦ , and 0.87 ◦ , respectively. Additionally, 97.7% of the errors in airspeed were within 1 m/s of the MHP, while 93.8% and 87.3% of the angle of attack and sideslip errors were within 1 ◦ . Flight tests show that a FADS can be calibrated in flight, and is an effective method for measuring the aircraft-relative wind from a small UAS. Advisors/Committee Members: Brian M. Argrow, Gijs de Boer, Nisar Ahmed, Alireza Doostan, John Farnsworth.

Subjects/Keywords: computational fluid dynamics; flush airdata system; neural networks; sUAS; unmanned aircraft systems; wind measurements; Aeronautical Vehicles; Aerospace Engineering

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APA (6^th Edition):

Laurence, Roger Jean, I. (2017). Suas Wind Sensing with Computational Fluid Dynamics and a Distributed Flush Airdata System. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/179

Chicago Manual of Style (16^th Edition):

Laurence, Roger Jean, III. “Suas Wind Sensing with Computational Fluid Dynamics and a Distributed Flush Airdata System.” 2017. Doctoral Dissertation, University of Colorado. Accessed January 20, 2020. https://scholar.colorado.edu/asen_gradetds/179.

MLA Handbook (7^th Edition):

Laurence, Roger Jean, III. “Suas Wind Sensing with Computational Fluid Dynamics and a Distributed Flush Airdata System.” 2017. Web. 20 Jan 2020.

Vancouver:

Laurence, Roger Jean I. Suas Wind Sensing with Computational Fluid Dynamics and a Distributed Flush Airdata System. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2020 Jan 20]. Available from: https://scholar.colorado.edu/asen_gradetds/179.

Council of Science Editors:

Laurence, Roger Jean I. Suas Wind Sensing with Computational Fluid Dynamics and a Distributed Flush Airdata System. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/179

Brigham Young University

9. Carlson, Daniel Clarke. Aerial Recovery of Micro Air Vehicles: Orbit Estimation and Tracking.

Degree: MS, 2010, Brigham Young University

URL: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3398&context=etd

► Aerial recovery of autonomous micro air vehicles (MAVs) presents many unique challenges due to the difference in size and speed of the recovery vehicle… (more)

Subjects/Keywords: aerial recovery; unmanned air vehicles; micro air vehicles; towed cable systems; orbit estimation; orbit tracking; Mechanical Engineering

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APA (6^th Edition):

Carlson, D. C. (2010). Aerial Recovery of Micro Air Vehicles: Orbit Estimation and Tracking. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3398&context=etd

Chicago Manual of Style (16^th Edition):

Carlson, Daniel Clarke. “Aerial Recovery of Micro Air Vehicles: Orbit Estimation and Tracking.” 2010. Masters Thesis, Brigham Young University. Accessed January 20, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3398&context=etd.

MLA Handbook (7^th Edition):

Carlson, Daniel Clarke. “Aerial Recovery of Micro Air Vehicles: Orbit Estimation and Tracking.” 2010. Web. 20 Jan 2020.

Vancouver:

Carlson DC. Aerial Recovery of Micro Air Vehicles: Orbit Estimation and Tracking. [Internet] [Masters thesis]. Brigham Young University; 2010. [cited 2020 Jan 20]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3398&context=etd.

Council of Science Editors:

Carlson DC. Aerial Recovery of Micro Air Vehicles: Orbit Estimation and Tracking. [Masters Thesis]. Brigham Young University; 2010. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3398&context=etd

University of Kentucky

10. Sparks, Jeremy Ryan. EXPERIMENTAL FLOW VISUALIZATION FOR CORRUGATED AIRFOILS AT LOW REYNOLDS NUMBER INCLUDING DEVELOPMENT OF A PITCH AND PLUNGE FIXTURE.

Degree: 2011, University of Kentucky

URL: http://uknowledge.uky.edu/gradschool_theses/141

► Micro Air Vehicles (MAV’s) have small size and extreme maneuverability which makes them ideal for surveillance. Propulsion mechanisms include propellers, rotors, and flapping airfoils. Flapping… (more)

Subjects/Keywords: CORRUGATED AIRFOIL; DRAGONFLY; LOW REYNOLDS NUMBER; MICRO AIR VEHICLES (MAV’s); PITCH AND PLUNGE; Aeronautical Vehicles; Mechanical Engineering

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APA (6^th Edition):

Sparks, J. R. (2011). EXPERIMENTAL FLOW VISUALIZATION FOR CORRUGATED AIRFOILS AT LOW REYNOLDS NUMBER INCLUDING DEVELOPMENT OF A PITCH AND PLUNGE FIXTURE. (Masters Thesis). University of Kentucky. Retrieved from http://uknowledge.uky.edu/gradschool_theses/141

Chicago Manual of Style (16^th Edition):

Sparks, Jeremy Ryan. “EXPERIMENTAL FLOW VISUALIZATION FOR CORRUGATED AIRFOILS AT LOW REYNOLDS NUMBER INCLUDING DEVELOPMENT OF A PITCH AND PLUNGE FIXTURE.” 2011. Masters Thesis, University of Kentucky. Accessed January 20, 2020. http://uknowledge.uky.edu/gradschool_theses/141.

MLA Handbook (7^th Edition):

Sparks, Jeremy Ryan. “EXPERIMENTAL FLOW VISUALIZATION FOR CORRUGATED AIRFOILS AT LOW REYNOLDS NUMBER INCLUDING DEVELOPMENT OF A PITCH AND PLUNGE FIXTURE.” 2011. Web. 20 Jan 2020.

Vancouver:

Sparks JR. EXPERIMENTAL FLOW VISUALIZATION FOR CORRUGATED AIRFOILS AT LOW REYNOLDS NUMBER INCLUDING DEVELOPMENT OF A PITCH AND PLUNGE FIXTURE. [Internet] [Masters thesis]. University of Kentucky; 2011. [cited 2020 Jan 20]. Available from: http://uknowledge.uky.edu/gradschool_theses/141.

Council of Science Editors:

Sparks JR. EXPERIMENTAL FLOW VISUALIZATION FOR CORRUGATED AIRFOILS AT LOW REYNOLDS NUMBER INCLUDING DEVELOPMENT OF A PITCH AND PLUNGE FIXTURE. [Masters Thesis]. University of Kentucky; 2011. Available from: http://uknowledge.uky.edu/gradschool_theses/141

Embry-Riddle Aeronautical University

11. Scheppa, Michael D. Preliminary Design of an Asteroid Hopping Mission.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2011, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/122

► In 2010, NASA announced that its new vision is to support private space launch operations. It is anticipated that this new direction will create… (more)

▼ In 2010, NASA announced that its new vision is to support private space launch operations. It is anticipated that this new direction will create the need for new and innovative ideas that push the current boundaries of space exploration and contain the promise of substantial gain, both in research and capital. The purpose of the study is to plan and estimate the feasibility of a mission to visit a number of near Earth asteroids (NEAs). The mission would take place before the end of the 21st century, and would only use commercially available technology. Throughout the mission design process, while holding astronaut safety paramount, it was the goal to maximize the return while keeping the cost to a minimum. A mission of the nature would appeal to the private space industry because it could be easily adapted and set into motion. The mission design was divided into three main parts; mission timeline, vehicle design and power sources, with emphasis on nuclear and solar electric power, were investigated. The timeline and associated trajectories were initially selected using a numerical estimation and then optimized using Satellite Tool Kit (STK) 9.s's Design Explorer Optimizer [1]. Next, the spacecraft was design using commercially available parts that would support the mission requirements. The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) was and instrumental piece in maximizing the number of NEAs visited. Once the spacecraft was designed, acceptable power supply options were investigated. The VASIMR VX-200 requires 200 kilowatts of power to maintain thrust. This creates the need for a substantial power supply that consists of either a nuclear reactor of massive solar arrays. STK 9.1's Design Explorer Optimizer was able to create a mission time line that allowed for the exploration of seven NEAs in under two years, while keeping the total mission ΔV under 71 kilometers per second. Based on these initial findings, it is determined that a mission of this nature is feasible and would could greatly benefit the private space industry.

Subjects/Keywords: Aeronautical Vehicles; Aerospace Engineering; Space Vehicles

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APA (6^th Edition):

Scheppa, M. D. (2011). Preliminary Design of an Asteroid Hopping Mission. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/122

Chicago Manual of Style (16^th Edition):

Scheppa, Michael D. “Preliminary Design of an Asteroid Hopping Mission.” 2011. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 20, 2020. https://commons.erau.edu/edt/122.

MLA Handbook (7^th Edition):

Scheppa, Michael D. “Preliminary Design of an Asteroid Hopping Mission.” 2011. Web. 20 Jan 2020.

Vancouver:

Scheppa MD. Preliminary Design of an Asteroid Hopping Mission. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2011. [cited 2020 Jan 20]. Available from: https://commons.erau.edu/edt/122.

Council of Science Editors:

Scheppa MD. Preliminary Design of an Asteroid Hopping Mission. [Masters Thesis]. Embry-Riddle Aeronautical University; 2011. Available from: https://commons.erau.edu/edt/122

Brigham Young University

12. Yu, Huili. Vision-based Path Planning, Collision Avoidance, and Target Tracking for Unmanned Air and Ground Vehicles in Urban Environments.

Degree: PhD, 2011, Brigham Young University

URL: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4080&context=etd

► Unmanned vehicle systems, specifically Unmanned Air Vehicles (UAVs) and Unmanned Ground Vehicles (UGVs) have found potential use in both military and civilian applications. For many… (more)

▼ Unmanned vehicle systems, specifically Unmanned Air Vehicles (UAVs) and Unmanned Ground Vehicles (UGVs) have found potential use in both military and civilian applications. For many applications, unmanned vehicle systems are required to navigate in urban environments where obstacles with various types and sizes exist. The main contribution of this research is to offer vision-based path planning, collision avoidance, and target tracking strategies for Unmanned Air and Ground vehicles operating in urban environments. Two vision-based local-level frame mapping and planning techniques are first developed for Miniature Air Vehicles (MAVs). The techniques build maps and plan paths in the local-level frame of MAVs directly using the camera measurements without transforming to the inertial frame. Using a depth map of an environment obtained by computer vision methods, the first technique employs an extended Kalman Filter (EKF) to estimate the range, azimuth to, and height of obstacles, and constructs local spherical maps around MAVs. Based on the maps, the Rapidly-Exploring Random Tree (RRT) algorithm is used to plan collision-free Dubins paths. The second technique constructs local multi-resolution maps using an occupancy grid, which give higher resolution to the areas that are close to MAVs and give lower resolution to the areas that are far away. The maps are built using a log-polar representation. The two planning techniques are demonstrated in simulation and flight tests. Based on the observation that a camera does not provide accurate time-to-collision (TTC) measurements, two and three dimensional observability-based planning algorithms are explored. The techniques estimate both TTC and bearing using bearing-only measurements. A nonlinear observability analysis of state estimation process is conducted to obtain the conditions for complete observability of the system. Using the conditions, the observability-based planning algorithms are designed to minimize the estimation uncertainties while simultaneously avoiding collisions. The two dimensional planning algorithm parameterizes an obstacle using TTC and azimuth, and constructs local polar maps. The three dimensional planning algorithm parameterizes an obstacle using inverse TTC, azimuth, and elevation, and constructs local spherical maps. The algorithms are demonstrated in simulation. Lastly, a probabilistic path planning algorithm is developed for tracking a moving target in urban environments using UAVs and UGVs. The algorithm takes into account occlusions due to obstacles. It models the target using a dynamic occupancy grid and updates the target location using a Bayesian filter. Based on the target's current and probable future locations, a decentralized path planning algorithm is designed to generate suboptimal paths that maximize the sum of the joint probability of detection for all vehicles over a finite look-ahead horizon. Results demonstrate the planning algorithm is successful in solving the moving target tracking problem in urban environments.

Subjects/Keywords: path planning; collision avoidance; target tracking; unmanned air and ground vehicles; Electrical and Computer Engineering

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APA (6^th Edition):

Yu, H. (2011). Vision-based Path Planning, Collision Avoidance, and Target Tracking for Unmanned Air and Ground Vehicles in Urban Environments. (Doctoral Dissertation). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4080&context=etd

Chicago Manual of Style (16^th Edition):

Yu, Huili. “Vision-based Path Planning, Collision Avoidance, and Target Tracking for Unmanned Air and Ground Vehicles in Urban Environments.” 2011. Doctoral Dissertation, Brigham Young University. Accessed January 20, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4080&context=etd.

MLA Handbook (7^th Edition):

Yu, Huili. “Vision-based Path Planning, Collision Avoidance, and Target Tracking for Unmanned Air and Ground Vehicles in Urban Environments.” 2011. Web. 20 Jan 2020.

Vancouver:

Yu H. Vision-based Path Planning, Collision Avoidance, and Target Tracking for Unmanned Air and Ground Vehicles in Urban Environments. [Internet] [Doctoral dissertation]. Brigham Young University; 2011. [cited 2020 Jan 20]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4080&context=etd.

Council of Science Editors:

Yu H. Vision-based Path Planning, Collision Avoidance, and Target Tracking for Unmanned Air and Ground Vehicles in Urban Environments. [Doctoral Dissertation]. Brigham Young University; 2011. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4080&context=etd

ETH Zürich

13. Oung, Raymond. The Distributed Flight Array.

Degree: 2013, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/66837

Subjects/Keywords: KOOPERIERENDE ROBOTER; COOPERATE ROBOTS; MODULAR SYSTEM (MECHANICAL ENGINEERING); UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); BAUKASTENSYSTEM (MASCHINENBAU); UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); info:eu-repo/classification/ddc/621.3; Electric engineering

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APA (6^th Edition):

Oung, R. (2013). The Distributed Flight Array. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/66837

Chicago Manual of Style (16^th Edition):

Oung, Raymond. “The Distributed Flight Array.” 2013. Doctoral Dissertation, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/66837.

MLA Handbook (7^th Edition):

Oung, Raymond. “The Distributed Flight Array.” 2013. Web. 20 Jan 2020.

Vancouver:

Oung R. The Distributed Flight Array. [Internet] [Doctoral dissertation]. ETH Zürich; 2013. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/66837.

Council of Science Editors:

Oung R. The Distributed Flight Array. [Doctoral Dissertation]. ETH Zürich; 2013. Available from: http://hdl.handle.net/20.500.11850/66837

ETH Zürich

14. Ammar, Mirjan. Aerial Construction: Robotic Fabrication of Tensile Structures with Flying Machines.

Degree: 2016, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/130425

Subjects/Keywords: KONSTRUKTION IM HOCHBAU (ARCHITEKTUR); BAUWESEN (GEBAUTE UMWELT); HUBSCHRAUBER, QUADROKOPTER, MULTIKOPTER (LUFTFAHRTTECHNIK); UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); BUILDING CONSTRUCTION (ARCHITECTURE); BUILDING (BUILT ENVIRONMENT); HELICOPTERS, QUADROTORS, MULTIROTORS (AERONAUTICAL ENGINEERING); UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); info:eu-repo/classification/ddc/621.3; Electric engineering

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APA (6^th Edition):

Ammar, M. (2016). Aerial Construction: Robotic Fabrication of Tensile Structures with Flying Machines. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/130425

Chicago Manual of Style (16^th Edition):

Ammar, Mirjan. “Aerial Construction: Robotic Fabrication of Tensile Structures with Flying Machines.” 2016. Doctoral Dissertation, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/130425.

MLA Handbook (7^th Edition):

Ammar, Mirjan. “Aerial Construction: Robotic Fabrication of Tensile Structures with Flying Machines.” 2016. Web. 20 Jan 2020.

Vancouver:

Ammar M. Aerial Construction: Robotic Fabrication of Tensile Structures with Flying Machines. [Internet] [Doctoral dissertation]. ETH Zürich; 2016. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/130425.

Council of Science Editors:

Ammar M. Aerial Construction: Robotic Fabrication of Tensile Structures with Flying Machines. [Doctoral Dissertation]. ETH Zürich; 2016. Available from: http://hdl.handle.net/20.500.11850/130425

University of Kentucky

15. Thamann, Michael. AERODYNAMICS AND CONTROL OF A DEPLOYABLE WING UAV FOR AUTONOMOUS FLIGHT.

Degree: 2012, University of Kentucky

URL: http://uknowledge.uky.edu/me_etds/18

► UAV development and usage has increased dramatically in the last 15 years. In this time frame the potential has been realized for deployable UAVs to… (more)

Subjects/Keywords: Unmanned Aerial Vehicle; Inflatable Wing; Bumpy Airfoil; Wing Shaping; Autonomous Flight; Acoustics, Dynamics, and Controls; Aerodynamics and Fluid Mechanics; Aeronautical Vehicles; Aerospace Engineering; Mechanical Engineering

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APA (6^th Edition):

Thamann, M. (2012). AERODYNAMICS AND CONTROL OF A DEPLOYABLE WING UAV FOR AUTONOMOUS FLIGHT. (Masters Thesis). University of Kentucky. Retrieved from http://uknowledge.uky.edu/me_etds/18

Chicago Manual of Style (16^th Edition):

Thamann, Michael. “AERODYNAMICS AND CONTROL OF A DEPLOYABLE WING UAV FOR AUTONOMOUS FLIGHT.” 2012. Masters Thesis, University of Kentucky. Accessed January 20, 2020. http://uknowledge.uky.edu/me_etds/18.

MLA Handbook (7^th Edition):

Thamann, Michael. “AERODYNAMICS AND CONTROL OF A DEPLOYABLE WING UAV FOR AUTONOMOUS FLIGHT.” 2012. Web. 20 Jan 2020.

Vancouver:

Thamann M. AERODYNAMICS AND CONTROL OF A DEPLOYABLE WING UAV FOR AUTONOMOUS FLIGHT. [Internet] [Masters thesis]. University of Kentucky; 2012. [cited 2020 Jan 20]. Available from: http://uknowledge.uky.edu/me_etds/18.

Council of Science Editors:

Thamann M. AERODYNAMICS AND CONTROL OF A DEPLOYABLE WING UAV FOR AUTONOMOUS FLIGHT. [Masters Thesis]. University of Kentucky; 2012. Available from: http://uknowledge.uky.edu/me_etds/18

ETH Zürich

16. Schmid, Korbinian N. Scalable, Multi-Sensor Aided Inertial Navigation for Agile Robots.

Degree: 2015, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/102248

Subjects/Keywords: KALMAN-FILTER (THEORIE DER REGELUNGSSYSTEME); INERTIAL NAVIGATION SYSTEMS (AERONAUTICAL ENGINEERING); HUBSCHRAUBER, QUADROKOPTER, MULTIKOPTER (LUFTFAHRTTECHNIK); FLUGNAVIGATION; UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); TRÄGHEITSNAVIGATION (LUFTFAHRTTECHNIK); AIR NAVIGATION; KALMAN FILTERING (CONTROL SYSTEMS THEORY); HELICOPTERS, QUADROTORS, MULTIROTORS (AERONAUTICAL ENGINEERING); UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); info:eu-repo/classification/ddc/621.3; Electric engineering

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APA (6^th Edition):

Schmid, K. N. (2015). Scalable, Multi-Sensor Aided Inertial Navigation for Agile Robots. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/102248

Chicago Manual of Style (16^th Edition):

Schmid, Korbinian N. “Scalable, Multi-Sensor Aided Inertial Navigation for Agile Robots.” 2015. Doctoral Dissertation, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/102248.

MLA Handbook (7^th Edition):

Schmid, Korbinian N. “Scalable, Multi-Sensor Aided Inertial Navigation for Agile Robots.” 2015. Web. 20 Jan 2020.

Vancouver:

Schmid KN. Scalable, Multi-Sensor Aided Inertial Navigation for Agile Robots. [Internet] [Doctoral dissertation]. ETH Zürich; 2015. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/102248.

Council of Science Editors:

Schmid KN. Scalable, Multi-Sensor Aided Inertial Navigation for Agile Robots. [Doctoral Dissertation]. ETH Zürich; 2015. Available from: http://hdl.handle.net/20.500.11850/102248

Brigham Young University

17. Ready, Bryce Benson. Filtering Techniques for Pose Estimation with Applications to Unmanned Air Vehicles.

Degree: PhD, 2012, Brigham Young University

URL: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4489&context=etd

► This work presents two novel methods of estimating the state of a dynamic system in a Kalman Filtering framework. The first is an application specific… (more)

Subjects/Keywords: Riemannian manifold; Kalman filter; unmanned air vehicles; homography; image registration; direct image registration; visual odometry; Electrical and Computer Engineering

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APA (6^th Edition):

Ready, B. B. (2012). Filtering Techniques for Pose Estimation with Applications to Unmanned Air Vehicles. (Doctoral Dissertation). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4489&context=etd

Chicago Manual of Style (16^th Edition):

Ready, Bryce Benson. “Filtering Techniques for Pose Estimation with Applications to Unmanned Air Vehicles.” 2012. Doctoral Dissertation, Brigham Young University. Accessed January 20, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4489&context=etd.

MLA Handbook (7^th Edition):

Ready, Bryce Benson. “Filtering Techniques for Pose Estimation with Applications to Unmanned Air Vehicles.” 2012. Web. 20 Jan 2020.

Vancouver:

Ready BB. Filtering Techniques for Pose Estimation with Applications to Unmanned Air Vehicles. [Internet] [Doctoral dissertation]. Brigham Young University; 2012. [cited 2020 Jan 20]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4489&context=etd.

Council of Science Editors:

Ready BB. Filtering Techniques for Pose Estimation with Applications to Unmanned Air Vehicles. [Doctoral Dissertation]. Brigham Young University; 2012. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4489&context=etd

Embry-Riddle Aeronautical University

18. Hamada, Said S. Development of a Small Unmanned Aerial Vehicle Longitudinal Model for Future Flutter Testing.

Degree: MSin Aerospace Engineering, Graduate Studies, 2018, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/395

► This thesis presents the system identification of the longitudinal motion of a small unmanned aerial vehicle with flexible characteristics. The unmanned aerial vehicle of… (more)

Subjects/Keywords: Aeronautical Vehicles

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APA (6^th Edition):

Hamada, S. S. (2018). Development of a Small Unmanned Aerial Vehicle Longitudinal Model for Future Flutter Testing. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/395

Chicago Manual of Style (16^th Edition):

Hamada, Said S. “Development of a Small Unmanned Aerial Vehicle Longitudinal Model for Future Flutter Testing.” 2018. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 20, 2020. https://commons.erau.edu/edt/395.

MLA Handbook (7^th Edition):

Hamada, Said S. “Development of a Small Unmanned Aerial Vehicle Longitudinal Model for Future Flutter Testing.” 2018. Web. 20 Jan 2020.

Vancouver:

Hamada SS. Development of a Small Unmanned Aerial Vehicle Longitudinal Model for Future Flutter Testing. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Jan 20]. Available from: https://commons.erau.edu/edt/395.

Council of Science Editors:

Hamada SS. Development of a Small Unmanned Aerial Vehicle Longitudinal Model for Future Flutter Testing. [Masters Thesis]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/395

Embry-Riddle Aeronautical University

19. Pedroza, Natalie Ramos. Robust Nonlinear Estimation and Control Applications using Synthetic Jet Actuators.

Degree: PhD, Doctoral Studies, 2018, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/403

► Limit cycle oscillations (LCO), also known as utter, cause significant challenges in flight control of small unmanned aerial vehicles (SUAVs), and could potentially lead… (more)

▼ Limit cycle oscillations (LCO), also known as utter, cause significant challenges in flight control of small unmanned aerial vehicles (SUAVs), and could potentially lead to structural damage and catastrophic failures. LCO can be described as vibrational motions in the rocking, pitching and plunging displacements of an aircraft wing. To address this, the use of synthetic jet actuators (SJAs) in UAV flight control systems is becoming popular as a practical alternative and to mechanical deflection surfaces. Synthetic jet actuators are promising tools for LCO suppression systems in small UAVs due to their small size, ease of operation, and low cost. Uncertainties inherent in the dynamics of the synthetic jet actuators present significant challenges in the synthetic jet actuator-based control design. Specifically, the input-output characteristic (voltage-virtual deflection angle relationship) of the synthetic jet actuators is nonlinear and contains parametric uncertainty. Further control design challenges exist in situations where multiple actuators lose effectiveness. This dissertation focuses on the suppression of limit cycle oscillations on small unmanned air vehicles using synthetic jet actuators. A brief description on how wind gust affects aircraft tracking control is presented. It shows an extension to a paper by adding the wind gust model to the system while also varying the uncertain synthetic jet actuator parameters using a Monte Carlo method. Next, a robust nonlinear control method is presented, which achieves simultaneous aircraft tracking control and limit cycle oscillation suppression using these synthetic jet actuators and a robust controller. Following that, a nonlinear LCO regulation method is presented, which uses a bank of dynamic filters to eliminate the need for pitching and plunging LCO rate measurements. Finally, an alternative method of LCO regulation control is presented, which utilizes a sliding mode observer in lieu of a bank of filters to estimate the pitching and plunging LCO rates.

Subjects/Keywords: Aeronautical Vehicles

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APA (6^th Edition):

Pedroza, N. R. (2018). Robust Nonlinear Estimation and Control Applications using Synthetic Jet Actuators. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/403

Chicago Manual of Style (16^th Edition):

Pedroza, Natalie Ramos. “Robust Nonlinear Estimation and Control Applications using Synthetic Jet Actuators.” 2018. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed January 20, 2020. https://commons.erau.edu/edt/403.

MLA Handbook (7^th Edition):

Pedroza, Natalie Ramos. “Robust Nonlinear Estimation and Control Applications using Synthetic Jet Actuators.” 2018. Web. 20 Jan 2020.

Vancouver:

Pedroza NR. Robust Nonlinear Estimation and Control Applications using Synthetic Jet Actuators. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2018. [cited 2020 Jan 20]. Available from: https://commons.erau.edu/edt/403.

Council of Science Editors:

Pedroza NR. Robust Nonlinear Estimation and Control Applications using Synthetic Jet Actuators. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2018. Available from: https://commons.erau.edu/edt/403

Embry-Riddle Aeronautical University

20. Memon, Muhammad Wasif. Fuel Efficient Control Design and Constrained Motion Analysis for Spacecraft Coloumb Formation in Elliptic Chief Orbits.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2019, Embry-Riddle Aeronautical University

URL: https://commons.erau.edu/edt/490

► The use of Coulomb force has been analyzed in recent years to provide propulsion in space for various applications. Coulomb formation can also be… (more)

Subjects/Keywords: Aeronautical Vehicles

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APA (6^th Edition):

Memon, M. W. (2019). Fuel Efficient Control Design and Constrained Motion Analysis for Spacecraft Coloumb Formation in Elliptic Chief Orbits. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/490

Chicago Manual of Style (16^th Edition):

Memon, Muhammad Wasif. “Fuel Efficient Control Design and Constrained Motion Analysis for Spacecraft Coloumb Formation in Elliptic Chief Orbits.” 2019. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 20, 2020. https://commons.erau.edu/edt/490.

MLA Handbook (7^th Edition):

Memon, Muhammad Wasif. “Fuel Efficient Control Design and Constrained Motion Analysis for Spacecraft Coloumb Formation in Elliptic Chief Orbits.” 2019. Web. 20 Jan 2020.

Vancouver:

Memon MW. Fuel Efficient Control Design and Constrained Motion Analysis for Spacecraft Coloumb Formation in Elliptic Chief Orbits. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2019. [cited 2020 Jan 20]. Available from: https://commons.erau.edu/edt/490.

Council of Science Editors:

Memon MW. Fuel Efficient Control Design and Constrained Motion Analysis for Spacecraft Coloumb Formation in Elliptic Chief Orbits. [Masters Thesis]. Embry-Riddle Aeronautical University; 2019. Available from: https://commons.erau.edu/edt/490

University of Central Florida

21. DeJong, Paul. Coalition Formation In Multi-agent Uav Systems.

Degree: 2005, University of Central Florida

URL: https://stars.library.ucf.edu/etd/303

► Coalitions are collections of agents that join together to solve a common problem that either cannot be solved individually or can be solved more efficiently… (more)

Subjects/Keywords: Coalition Formation; Coalitions; Coalition; Agents; Agent; Mutli-Agent; Multi-Agent Systems; Unmanned Air Vehicle; Unmanned Air Vehicles; Unmanned Aerial Vehicle; Unmanned Aerial Vehicles; UAV; Computer Engineering; Engineering

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APA (6^th Edition):

DeJong, P. (2005). Coalition Formation In Multi-agent Uav Systems. (Masters Thesis). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/303

Chicago Manual of Style (16^th Edition):

DeJong, Paul. “Coalition Formation In Multi-agent Uav Systems.” 2005. Masters Thesis, University of Central Florida. Accessed January 20, 2020. https://stars.library.ucf.edu/etd/303.

MLA Handbook (7^th Edition):

DeJong, Paul. “Coalition Formation In Multi-agent Uav Systems.” 2005. Web. 20 Jan 2020.

Vancouver:

DeJong P. Coalition Formation In Multi-agent Uav Systems. [Internet] [Masters thesis]. University of Central Florida; 2005. [cited 2020 Jan 20]. Available from: https://stars.library.ucf.edu/etd/303.

Council of Science Editors:

DeJong P. Coalition Formation In Multi-agent Uav Systems. [Masters Thesis]. University of Central Florida; 2005. Available from: https://stars.library.ucf.edu/etd/303

ETH Zürich

22. Schneider, Daniel. Path Planning for Fixed-Wing Unmanned Aerial Vehicles.

Degree: 2016, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/116625

Subjects/Keywords: MOTION PLANNING + MOTION COURSE + TRAJECTORY PLANNING (ROBOTICS); BEWEGUNGSVERLAUF + BEWEGUNGSABLAUF + BAHNPLANUNG (ROBOTIK); UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/621.3; Engineering & allied operations; Electric engineering

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APA (6^th Edition):

Schneider, D. (2016). Path Planning for Fixed-Wing Unmanned Aerial Vehicles. (Thesis). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/116625

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Schneider, Daniel. “Path Planning for Fixed-Wing Unmanned Aerial Vehicles.” 2016. Thesis, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/116625.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Schneider, Daniel. “Path Planning for Fixed-Wing Unmanned Aerial Vehicles.” 2016. Web. 20 Jan 2020.

Vancouver:

Schneider D. Path Planning for Fixed-Wing Unmanned Aerial Vehicles. [Internet] [Thesis]. ETH Zürich; 2016. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/116625.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Schneider D. Path Planning for Fixed-Wing Unmanned Aerial Vehicles. [Thesis]. ETH Zürich; 2016. Available from: http://hdl.handle.net/20.500.11850/116625

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

ETH Zürich

23. Meier, Lorenz. Fast and robust localization and mapping on micro air vehicles.

Degree: 2011, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/152627

Subjects/Keywords: UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); MIKROTECHNIK; FLUGZEUGORTUNG MITTELS RADAR (RADARTECHNIK); OPTISCHE ABBILDUNG; UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); MICROTECHNOLOGY; AIRCRAFT DETECTION BY MEANS OF RADAR (RADAR ENGINEERING); OPTICAL IMAGING; info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA (6^th Edition):

Meier, L. (2011). Fast and robust localization and mapping on micro air vehicles. (Thesis). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/152627

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Meier, Lorenz. “Fast and robust localization and mapping on micro air vehicles.” 2011. Thesis, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/152627.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Meier, Lorenz. “Fast and robust localization and mapping on micro air vehicles.” 2011. Web. 20 Jan 2020.

Vancouver:

Meier L. Fast and robust localization and mapping on micro air vehicles. [Internet] [Thesis]. ETH Zürich; 2011. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/152627.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Meier L. Fast and robust localization and mapping on micro air vehicles. [Thesis]. ETH Zürich; 2011. Available from: http://hdl.handle.net/20.500.11850/152627

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

ETH Zürich

24. Nussberger, Andreas. Aerial Object Tracking from an Airborne Platform.

Degree: 2015, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/113116

Subjects/Keywords: COMPUTER VISION + SCENE UNDERSTANDING (ARTIFICIAL INTELLIGENCE); DIGITALE BILDVERARBEITUNG; DIGITAL IMAGE PROCESSING; COMPUTERVISION (KÜNSTLICHE INTELLIGENZ); UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA (6^th Edition):

Nussberger, A. (2015). Aerial Object Tracking from an Airborne Platform. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/113116

Chicago Manual of Style (16^th Edition):

Nussberger, Andreas. “Aerial Object Tracking from an Airborne Platform.” 2015. Doctoral Dissertation, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/113116.

MLA Handbook (7^th Edition):

Nussberger, Andreas. “Aerial Object Tracking from an Airborne Platform.” 2015. Web. 20 Jan 2020.

Vancouver:

Nussberger A. Aerial Object Tracking from an Airborne Platform. [Internet] [Doctoral dissertation]. ETH Zürich; 2015. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/113116.

Council of Science Editors:

Nussberger A. Aerial Object Tracking from an Airborne Platform. [Doctoral Dissertation]. ETH Zürich; 2015. Available from: http://hdl.handle.net/20.500.11850/113116

Virginia Tech

25. Kakar, Jaber Ahmad. UAV Communications: Spectral Requirements, MAV and SUAV Channel Modeling, OFDM Waveform Parameters, Performance and Spectrum Management.

Degree: MS, Electrical and Computer Engineering, 2015, Virginia Tech

URL: http://hdl.handle.net/10919/53512

► Unmanned Aerial Vehicles (UAV) are expected to be deployed both by government and industry. Rules for integrating commercial UAVs into a nation's airspace still need… (more)

Subjects/Keywords: Unmanned Aerial Vehicles; OFDM; Spectrum Management; Air-to-Ground Channels

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APA (6^th Edition):

Kakar, J. A. (2015). UAV Communications: Spectral Requirements, MAV and SUAV Channel Modeling, OFDM Waveform Parameters, Performance and Spectrum Management. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/53512

Chicago Manual of Style (16^th Edition):

Kakar, Jaber Ahmad. “UAV Communications: Spectral Requirements, MAV and SUAV Channel Modeling, OFDM Waveform Parameters, Performance and Spectrum Management.” 2015. Masters Thesis, Virginia Tech. Accessed January 20, 2020. http://hdl.handle.net/10919/53512.

MLA Handbook (7^th Edition):

Kakar, Jaber Ahmad. “UAV Communications: Spectral Requirements, MAV and SUAV Channel Modeling, OFDM Waveform Parameters, Performance and Spectrum Management.” 2015. Web. 20 Jan 2020.

Vancouver:

Kakar JA. UAV Communications: Spectral Requirements, MAV and SUAV Channel Modeling, OFDM Waveform Parameters, Performance and Spectrum Management. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/10919/53512.

Council of Science Editors:

Kakar JA. UAV Communications: Spectral Requirements, MAV and SUAV Channel Modeling, OFDM Waveform Parameters, Performance and Spectrum Management. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/53512

University of Colorado

26. Howard, Micah A. Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems.

Degree: PhD, Aerospace Engineering Sciences, 2010, University of Colorado

URL: https://scholar.colorado.edu/asen_gradetds/9

► The design of supersonic and hypersonic aerospace vehicles is by nature a multi-disciplinary problem requiring the close integration of compressible fluid dynamics, heat transfer,… (more)

Subjects/Keywords: aerospace vehicles; aerothermoelastic behavior; thermal and structural performance; Aeronautical Vehicles; Aerospace Engineering; Space Vehicles

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Howard, M. A. (2010). Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/9

Chicago Manual of Style (16^th Edition):

Howard, Micah A. “Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems.” 2010. Doctoral Dissertation, University of Colorado. Accessed January 20, 2020. https://scholar.colorado.edu/asen_gradetds/9.

MLA Handbook (7^th Edition):

Howard, Micah A. “Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems.” 2010. Web. 20 Jan 2020.

Vancouver:

Howard MA. Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems. [Internet] [Doctoral dissertation]. University of Colorado; 2010. [cited 2020 Jan 20]. Available from: https://scholar.colorado.edu/asen_gradetds/9.

Council of Science Editors:

Howard MA. Finite Element Modeling and Optimization of High-Speed Aerothermoelastic Systems. [Doctoral Dissertation]. University of Colorado; 2010. Available from: https://scholar.colorado.edu/asen_gradetds/9

Indian Institute of Science

27. Manathara, Joel George. Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments.

Degree: 2011, Indian Institute of Science

URL: http://hdl.handle.net/2005/2360

► This thesis addresses the problems of collision avoidance and coalition formation of multiple UAVs in high density traffic environments, proposes simple and efficient algorithms as… (more)

▼ This thesis addresses the problems of collision avoidance and coalition formation of multiple UAVs in high density traffic environments, proposes simple and efficient algorithms as solutions, and discusses their applications in multiple UAV missions. First, the problem of collision avoidance among UAVs is considered and deconfliction algorithms are proposed. The efficacy of the proposed algorithms is tested using simulations involving random flights in high density traffic. Further, the proposed collision avoidance algorithms are implemented using realistic six degree of freedom UAV models. The studies in this thesis show that implementation of the proposed collision avoidance algorithms leads to a safer and efficient operational airspace occupied by multiple UAVs. Next, coalition formation in a search and prosecute mission involving a large number of UAVs and targets is considered. This problem is shown to be NP-hard and a sub-optimal but polynomial time coalition formation strategy is proposed. Simulations are carried out to show that this coalition formation algorithm works well. The coalition formation algorithm is then extended to handle situations where the UAVs have limited communication ranges. Finally, this thesis considers some multiple UAV missions that require the application of collision avoidance and coalition formation techniques. The problem of multiple UAV rendezvous is tackled by using (i) a consensus among the UAVs to attain rendezvous and (ii) the collision avoidance algorithm previously developed for safety. The thesis also considers a search and prosecute mission where the UAVs also have to avoid collisions among one another. In summary, the main contributions of this thesis include (a) novel collision avoidance algorithms, which are conceptually simple and easy to implement, for resolving path conflicts – both planar and three dimensional – in a high density traffic airspace with UAVs in free flight and (b) efficient coalition formation algorithms for search and prosecute task with large number of UAVs and targets where UAVs have limited communication ranges and targets are maneuvering. Simulations to evaluate the performance of algorithms based on these concepts to carry out realistic tasks by UAV swarms are also given. Advisors/Committee Members: Ghose, Debasish.

Subjects/Keywords: Unmanned Aerial vehicles - Collision Avoidance; Airplanes - Collision Avoidance; Air Traffic Control; Unmanned Aerial Vehicles - Coalition Formation; Airplane Collisions; Unmanned Aerial Vehicles - Collision Avoidance Algorithms; UAV Models; Coalition Formation; Astronautics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Manathara, J. G. (2011). Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2360

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Manathara, Joel George. “Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments.” 2011. Thesis, Indian Institute of Science. Accessed January 20, 2020. http://hdl.handle.net/2005/2360.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Manathara, Joel George. “Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments.” 2011. Web. 20 Jan 2020.

Vancouver:

Manathara JG. Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments. [Internet] [Thesis]. Indian Institute of Science; 2011. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/2005/2360.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Manathara JG. Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments. [Thesis]. Indian Institute of Science; 2011. Available from: http://hdl.handle.net/2005/2360

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Indian Institute of Science

28. Manathara, Joel George. Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments.

Degree: 2011, Indian Institute of Science

URL: http://etd.iisc.ernet.in/handle/2005/2360 ; http://etd.ncsi.iisc.ernet.in/abstracts/3034/G24876-Abs.pdf

► This thesis addresses the problems of collision avoidance and coalition formation of multiple UAVs in high density traffic environments, proposes simple and efficient algorithms as… (more)

▼ This thesis addresses the problems of collision avoidance and coalition formation of multiple UAVs in high density traffic environments, proposes simple and efficient algorithms as solutions, and discusses their applications in multiple UAV missions. First, the problem of collision avoidance among UAVs is considered and deconfliction algorithms are proposed. The efficacy of the proposed algorithms is tested using simulations involving random flights in high density traffic. Further, the proposed collision avoidance algorithms are implemented using realistic six degree of freedom UAV models. The studies in this thesis show that implementation of the proposed collision avoidance algorithms leads to a safer and efficient operational airspace occupied by multiple UAVs. Next, coalition formation in a search and prosecute mission involving a large number of UAVs and targets is considered. This problem is shown to be NP-hard and a sub-optimal but polynomial time coalition formation strategy is proposed. Simulations are carried out to show that this coalition formation algorithm works well. The coalition formation algorithm is then extended to handle situations where the UAVs have limited communication ranges. Finally, this thesis considers some multiple UAV missions that require the application of collision avoidance and coalition formation techniques. The problem of multiple UAV rendezvous is tackled by using (i) a consensus among the UAVs to attain rendezvous and (ii) the collision avoidance algorithm previously developed for safety. The thesis also considers a search and prosecute mission where the UAVs also have to avoid collisions among one another. In summary, the main contributions of this thesis include (a) novel collision avoidance algorithms, which are conceptually simple and easy to implement, for resolving path conflicts – both planar and three dimensional – in a high density traffic airspace with UAVs in free flight and (b) efficient coalition formation algorithms for search and prosecute task with large number of UAVs and targets where UAVs have limited communication ranges and targets are maneuvering. Simulations to evaluate the performance of algorithms based on these concepts to carry out realistic tasks by UAV swarms are also given. Advisors/Committee Members: Ghose, Debasish.

Subjects/Keywords: Unmanned Aerial vehicles - Collision Avoidance; Airplanes - Collision Avoidance; Air Traffic Control; Unmanned Aerial Vehicles - Coalition Formation; Airplane Collisions; Unmanned Aerial Vehicles - Collision Avoidance Algorithms; UAV Models; Coalition Formation; Astronautics

Record Details Similar Records Cite « Share

❌

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Manathara, J. G. (2011). Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2360 ; http://etd.ncsi.iisc.ernet.in/abstracts/3034/G24876-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Manathara, Joel George. “Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments.” 2011. Thesis, Indian Institute of Science. Accessed January 20, 2020. http://etd.iisc.ernet.in/handle/2005/2360 ; http://etd.ncsi.iisc.ernet.in/abstracts/3034/G24876-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Manathara, Joel George. “Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments.” 2011. Web. 20 Jan 2020.

Vancouver:

Manathara JG. Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments. [Internet] [Thesis]. Indian Institute of Science; 2011. [cited 2020 Jan 20]. Available from: http://etd.iisc.ernet.in/handle/2005/2360 ; http://etd.ncsi.iisc.ernet.in/abstracts/3034/G24876-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Manathara JG. Collision Avoidance And Coalition Formation Of Multiple Unmanned Aerial Vechicles In High Density Traffic Environments. [Thesis]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ernet.in/handle/2005/2360 ; http://etd.ncsi.iisc.ernet.in/abstracts/3034/G24876-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

ETH Zürich

29. Ducard, Guillaume Jacques Joseph. Fault-tolerant flight control and guidance systems for a small unmanned aerial vehicle.

Degree: 2007, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/4260

Subjects/Keywords: FAULT TREES (CONTROL SYSTEMS THEORY); NAVIGATIONSANLAGEN UND FLUGSTEUERUNGSANLAGEN (LUFTFAHRTTECHNIK); UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); NAVIGATION SYSTEMS AND FLIGHT CONTROL SYSTEMS (AERONAUTICAL ENGINEERING); FEHLERBÄUME (THEORIE DER REGELUNGSSYSTEME); UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/621.3; Engineering & allied operations; Electric engineering

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Ducard, G. J. J. (2007). Fault-tolerant flight control and guidance systems for a small unmanned aerial vehicle. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/4260

Chicago Manual of Style (16^th Edition):

Ducard, Guillaume Jacques Joseph. “Fault-tolerant flight control and guidance systems for a small unmanned aerial vehicle.” 2007. Doctoral Dissertation, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/4260.

MLA Handbook (7^th Edition):

Ducard, Guillaume Jacques Joseph. “Fault-tolerant flight control and guidance systems for a small unmanned aerial vehicle.” 2007. Web. 20 Jan 2020.

Vancouver:

Ducard GJJ. Fault-tolerant flight control and guidance systems for a small unmanned aerial vehicle. [Internet] [Doctoral dissertation]. ETH Zürich; 2007. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/4260.

Council of Science Editors:

Ducard GJJ. Fault-tolerant flight control and guidance systems for a small unmanned aerial vehicle. [Doctoral Dissertation]. ETH Zürich; 2007. Available from: http://hdl.handle.net/20.500.11850/4260

ETH Zürich

30. Asadpour, Mahdi. Location-aware Forwarding in Micro Aerial Vehicle Networks.

Degree: 2015, ETH Zürich

URL: http://hdl.handle.net/20.500.11850/106563

Subjects/Keywords: NETWORK PROTOCOLS + COMMUNICATION PROTOCOLS (COMPUTER SYSTEMS); NETZWERKPROTOKOLLE + KOMMUNIKATIONSPROTOKOLLE (COMPUTERSYSTEME); HUBSCHRAUBER, QUADROKOPTER, MULTIKOPTER (LUFTFAHRTTECHNIK); UNBEMANNTE FLUGZEUGE (LUFTFAHRTTECHNIK); HELICOPTERS, QUADROTORS, MULTIROTORS (AERONAUTICAL ENGINEERING); UNMANNED AIR VEHICLES (AERONAUTICAL ENGINEERING); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/621.3; Engineering & allied operations; Electric engineering

Record Details Similar Records Cite « Share

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Asadpour, M. (2015). Location-aware Forwarding in Micro Aerial Vehicle Networks. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/106563

Chicago Manual of Style (16^th Edition):

Asadpour, Mahdi. “Location-aware Forwarding in Micro Aerial Vehicle Networks.” 2015. Doctoral Dissertation, ETH Zürich. Accessed January 20, 2020. http://hdl.handle.net/20.500.11850/106563.

MLA Handbook (7^th Edition):

Asadpour, Mahdi. “Location-aware Forwarding in Micro Aerial Vehicle Networks.” 2015. Web. 20 Jan 2020.

Vancouver:

Asadpour M. Location-aware Forwarding in Micro Aerial Vehicle Networks. [Internet] [Doctoral dissertation]. ETH Zürich; 2015. [cited 2020 Jan 20]. Available from: http://hdl.handle.net/20.500.11850/106563.

Council of Science Editors:

Asadpour M. Location-aware Forwarding in Micro Aerial Vehicle Networks. [Doctoral Dissertation]. ETH Zürich; 2015. Available from: http://hdl.handle.net/20.500.11850/106563

Open Access Theses and Dissertations