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You searched for subject:(Flight vehicles). Showing records 1 – 30 of 99 total matches.

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University of Houston

1. Dam, Duy K. Analysis and Control of a Non-linear Flight Vehicle.

Degree: MS, Computer and Systems Engineering, 2014, University of Houston

 Unmanned flight vehicles have received considerable attention from researchers in multiple areas. They can be used as a research platform to evaluate new concepts in… (more)

Subjects/Keywords: Analysis; Controls; Quadcopter; Flight vehicles

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APA (6th Edition):

Dam, D. K. (2014). Analysis and Control of a Non-linear Flight Vehicle. (Masters Thesis). University of Houston. Retrieved from http://hdl.handle.net/10657/5671

Chicago Manual of Style (16th Edition):

Dam, Duy K. “Analysis and Control of a Non-linear Flight Vehicle.” 2014. Masters Thesis, University of Houston. Accessed January 26, 2021. http://hdl.handle.net/10657/5671.

MLA Handbook (7th Edition):

Dam, Duy K. “Analysis and Control of a Non-linear Flight Vehicle.” 2014. Web. 26 Jan 2021.

Vancouver:

Dam DK. Analysis and Control of a Non-linear Flight Vehicle. [Internet] [Masters thesis]. University of Houston; 2014. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/10657/5671.

Council of Science Editors:

Dam DK. Analysis and Control of a Non-linear Flight Vehicle. [Masters Thesis]. University of Houston; 2014. Available from: http://hdl.handle.net/10657/5671


Ryerson University

2. Li, Junquan. Intelligent Control of Satellite Formation Flying.

Degree: 2012, Ryerson University

 Small satellites flying in formation present a more efficient and affordable way of achieving the same or better performance than a large satellite because of… (more)

Subjects/Keywords: Space dynamics; Space vehicles  – Control systems; Space flight; Flight control; Artificial satellites  – Control systems

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

APA (6th Edition):

Li, J. (2012). Intelligent Control of Satellite Formation Flying. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A2347

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

Chicago Manual of Style (16th Edition):

Li, Junquan. “Intelligent Control of Satellite Formation Flying.” 2012. Thesis, Ryerson University. Accessed January 26, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A2347.

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

MLA Handbook (7th Edition):

Li, Junquan. “Intelligent Control of Satellite Formation Flying.” 2012. Web. 26 Jan 2021.

Vancouver:

Li J. Intelligent Control of Satellite Formation Flying. [Internet] [Thesis]. Ryerson University; 2012. [cited 2021 Jan 26]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2347.

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

Council of Science Editors:

Li J. Intelligent Control of Satellite Formation Flying. [Thesis]. Ryerson University; 2012. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2347

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


Ryerson University

3. Lin, Arthur Kar Leung. Control of spacecraft formation flying around asteroids.

Degree: 2014, Ryerson University

 There exist thousands of different minerals and other possible resources out in space. To exploit these resources and to further expand our knowledge of the… (more)

Subjects/Keywords: Space flight  – Mathematical models; Flight control; Asteroids; Space vehicles  – Control systems; Space industrialization; Navigation (Astronautics)

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APA (6th Edition):

Lin, A. K. L. (2014). Control of spacecraft formation flying around asteroids. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A4082

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

Chicago Manual of Style (16th Edition):

Lin, Arthur Kar Leung. “Control of spacecraft formation flying around asteroids.” 2014. Thesis, Ryerson University. Accessed January 26, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A4082.

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

MLA Handbook (7th Edition):

Lin, Arthur Kar Leung. “Control of spacecraft formation flying around asteroids.” 2014. Web. 26 Jan 2021.

Vancouver:

Lin AKL. Control of spacecraft formation flying around asteroids. [Internet] [Thesis]. Ryerson University; 2014. [cited 2021 Jan 26]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A4082.

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

Council of Science Editors:

Lin AKL. Control of spacecraft formation flying around asteroids. [Thesis]. Ryerson University; 2014. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A4082

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


Ryerson University

4. Wong, Frank Y.W. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.

Degree: 2009, Ryerson University

 This thesis examines the use of thrusters and solar sails for spacecraft formation keeping control at the Earth-Moon L4 point. Particular emphasis was placed on… (more)

Subjects/Keywords: Space trajectories; Guidance systems (Flight); Navigation (Astronautics); Space vehicles  – Propulsion systems; Space vehicles  – Attitude control systems; Flight control

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

APA (6th Edition):

Wong, F. Y. W. (2009). Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1550

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

Chicago Manual of Style (16th Edition):

Wong, Frank Y W. “Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.” 2009. Thesis, Ryerson University. Accessed January 26, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A1550.

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

MLA Handbook (7th Edition):

Wong, Frank Y W. “Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point.” 2009. Web. 26 Jan 2021.

Vancouver:

Wong FYW. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. [Internet] [Thesis]. Ryerson University; 2009. [cited 2021 Jan 26]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1550.

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

Council of Science Editors:

Wong FYW. Formation-Keeping Strategies At The Earth-Moon L4 Triangular Libration Point. [Thesis]. Ryerson University; 2009. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1550

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


Wright State University

5. Casey, Julian L. Analytical approach to multi-objective joint inference control for fixed wing unmanned aerial vehicles.

Degree: MSEE, Electrical Engineering, 2020, Wright State University

 Fixed-wing Unmanned Aerial Vehicles (UAVs) have been found highly useful in variousenvironments, including military and law enforcement. With the increased use offixed-wing UAVs, there becomes… (more)

Subjects/Keywords: Electrical Engineering; fixed wing unmanned aerial vehicles; unmanned aerial vehicles; UAVs; multi-objective flight

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

APA (6th Edition):

Casey, J. L. (2020). Analytical approach to multi-objective joint inference control for fixed wing unmanned aerial vehicles. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright160431245463856

Chicago Manual of Style (16th Edition):

Casey, Julian L. “Analytical approach to multi-objective joint inference control for fixed wing unmanned aerial vehicles.” 2020. Masters Thesis, Wright State University. Accessed January 26, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=wright160431245463856.

MLA Handbook (7th Edition):

Casey, Julian L. “Analytical approach to multi-objective joint inference control for fixed wing unmanned aerial vehicles.” 2020. Web. 26 Jan 2021.

Vancouver:

Casey JL. Analytical approach to multi-objective joint inference control for fixed wing unmanned aerial vehicles. [Internet] [Masters thesis]. Wright State University; 2020. [cited 2021 Jan 26]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright160431245463856.

Council of Science Editors:

Casey JL. Analytical approach to multi-objective joint inference control for fixed wing unmanned aerial vehicles. [Masters Thesis]. Wright State University; 2020. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright160431245463856


Cornell University

6. Pulla, Venkata Siva Prasad. Insect Powered Micro Air Vehicles And Centimeter Scale High Energy Density Pneumatic Sources.

Degree: PhD, Electrical Engineering, 2012, Cornell University

 The flight times of traditional Micro-Air-Vehicles (MAVs) are limited by low energy density of batteries at small scale. On the other hand insects outperform MAVs… (more)

Subjects/Keywords: Micro Air Vehicles; mems; Pheumatic actuators; Insect flight; composites

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

APA (6th Edition):

Pulla, V. S. P. (2012). Insect Powered Micro Air Vehicles And Centimeter Scale High Energy Density Pneumatic Sources. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/29506

Chicago Manual of Style (16th Edition):

Pulla, Venkata Siva Prasad. “Insect Powered Micro Air Vehicles And Centimeter Scale High Energy Density Pneumatic Sources.” 2012. Doctoral Dissertation, Cornell University. Accessed January 26, 2021. http://hdl.handle.net/1813/29506.

MLA Handbook (7th Edition):

Pulla, Venkata Siva Prasad. “Insect Powered Micro Air Vehicles And Centimeter Scale High Energy Density Pneumatic Sources.” 2012. Web. 26 Jan 2021.

Vancouver:

Pulla VSP. Insect Powered Micro Air Vehicles And Centimeter Scale High Energy Density Pneumatic Sources. [Internet] [Doctoral dissertation]. Cornell University; 2012. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/1813/29506.

Council of Science Editors:

Pulla VSP. Insect Powered Micro Air Vehicles And Centimeter Scale High Energy Density Pneumatic Sources. [Doctoral Dissertation]. Cornell University; 2012. Available from: http://hdl.handle.net/1813/29506


Brigham Young University

7. Clark, Spencer James. Sensor-Driven Hierarchical Path Planning for Unmanned Aerial Vehicles Using Canonical Tasks and Sensors.

Degree: MS, 2013, Brigham Young University

 Unmanned Aerial Vehicles (UAVs) are increasingly becoming economical platforms for carrying a variety of sensors. Building flight plans that place sensors properly, temporally and spatially,… (more)

Subjects/Keywords: Flight planning; unmanned aerial vehicles; UAVs; Computer Sciences

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

APA (6th Edition):

Clark, S. J. (2013). Sensor-Driven Hierarchical Path Planning for Unmanned Aerial Vehicles Using Canonical Tasks and Sensors. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4797&context=etd

Chicago Manual of Style (16th Edition):

Clark, Spencer James. “Sensor-Driven Hierarchical Path Planning for Unmanned Aerial Vehicles Using Canonical Tasks and Sensors.” 2013. Masters Thesis, Brigham Young University. Accessed January 26, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4797&context=etd.

MLA Handbook (7th Edition):

Clark, Spencer James. “Sensor-Driven Hierarchical Path Planning for Unmanned Aerial Vehicles Using Canonical Tasks and Sensors.” 2013. Web. 26 Jan 2021.

Vancouver:

Clark SJ. Sensor-Driven Hierarchical Path Planning for Unmanned Aerial Vehicles Using Canonical Tasks and Sensors. [Internet] [Masters thesis]. Brigham Young University; 2013. [cited 2021 Jan 26]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4797&context=etd.

Council of Science Editors:

Clark SJ. Sensor-Driven Hierarchical Path Planning for Unmanned Aerial Vehicles Using Canonical Tasks and Sensors. [Masters Thesis]. Brigham Young University; 2013. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4797&context=etd


University of Tennessee – Knoxville

8. Porcelli, Brittany Lane. Flight Test Optimization of Fixed-Wing and Rotary-Wing Unmanned Aerial Vehicles for Planetary Boundary Layer Research.

Degree: MS, Aerospace Engineering, 2020, University of Tennessee – Knoxville

 Current methods for atmospheric measurements, such as radiosondes, have limitations in providing adequate data collection in Earth’s planetary boundary layer. Technology has presented scientists with… (more)

Subjects/Keywords: Aerospace; Unmanned Aerial Vehicles; Flight Optimization; Space Institute; NOAA; Atmospheric Science

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

APA (6th Edition):

Porcelli, B. L. (2020). Flight Test Optimization of Fixed-Wing and Rotary-Wing Unmanned Aerial Vehicles for Planetary Boundary Layer Research. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/5612

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

Chicago Manual of Style (16th Edition):

Porcelli, Brittany Lane. “Flight Test Optimization of Fixed-Wing and Rotary-Wing Unmanned Aerial Vehicles for Planetary Boundary Layer Research.” 2020. Thesis, University of Tennessee – Knoxville. Accessed January 26, 2021. https://trace.tennessee.edu/utk_gradthes/5612.

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

MLA Handbook (7th Edition):

Porcelli, Brittany Lane. “Flight Test Optimization of Fixed-Wing and Rotary-Wing Unmanned Aerial Vehicles for Planetary Boundary Layer Research.” 2020. Web. 26 Jan 2021.

Vancouver:

Porcelli BL. Flight Test Optimization of Fixed-Wing and Rotary-Wing Unmanned Aerial Vehicles for Planetary Boundary Layer Research. [Internet] [Thesis]. University of Tennessee – Knoxville; 2020. [cited 2021 Jan 26]. Available from: https://trace.tennessee.edu/utk_gradthes/5612.

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

Council of Science Editors:

Porcelli BL. Flight Test Optimization of Fixed-Wing and Rotary-Wing Unmanned Aerial Vehicles for Planetary Boundary Layer Research. [Thesis]. University of Tennessee – Knoxville; 2020. Available from: https://trace.tennessee.edu/utk_gradthes/5612

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


University of Maryland

9. Badrya, Camli. CFD/Quasi-Steady Coupled Trim Analysis of Diptera-type Flapping Wing MAV in Steady Flight.

Degree: Aerospace Engineering, 2016, University of Maryland

 The nuances in flapping wing aerodynamics are not yet fully understood to the extent where concepts can be translated to practical designs. Trimmed flight is… (more)

Subjects/Keywords: Aerospace engineering; Aerodynamics; Computational Fluid Dynamics; Low Reynolds numbers; Micro Air Vehicles; Rotorcraft and vertical flight; Steady (trimmed) flight

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APA (6th Edition):

Badrya, C. (2016). CFD/Quasi-Steady Coupled Trim Analysis of Diptera-type Flapping Wing MAV in Steady Flight. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/19273

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

Chicago Manual of Style (16th Edition):

Badrya, Camli. “CFD/Quasi-Steady Coupled Trim Analysis of Diptera-type Flapping Wing MAV in Steady Flight.” 2016. Thesis, University of Maryland. Accessed January 26, 2021. http://hdl.handle.net/1903/19273.

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

MLA Handbook (7th Edition):

Badrya, Camli. “CFD/Quasi-Steady Coupled Trim Analysis of Diptera-type Flapping Wing MAV in Steady Flight.” 2016. Web. 26 Jan 2021.

Vancouver:

Badrya C. CFD/Quasi-Steady Coupled Trim Analysis of Diptera-type Flapping Wing MAV in Steady Flight. [Internet] [Thesis]. University of Maryland; 2016. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/1903/19273.

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

Council of Science Editors:

Badrya C. CFD/Quasi-Steady Coupled Trim Analysis of Diptera-type Flapping Wing MAV in Steady Flight. [Thesis]. University of Maryland; 2016. Available from: http://hdl.handle.net/1903/19273

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


Virginia Tech

10. Viswanath, Kamal. Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat.

Degree: PhD, Mechanical Engineering, 2013, Virginia Tech

 This dissertation broadly seeks to understand the effect different kinematic parameters, external forces, and dynamic wing conformation have on the fluid dynamics of flapping flight.… (more)

Subjects/Keywords: Computational fluid dynamics (CFD); Flapping Flight; Micro Air Vehicles; Flexible Wings; Bat Flight; Wind Gusts; Stroke Deviation

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

APA (6th Edition):

Viswanath, K. (2013). Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50825

Chicago Manual of Style (16th Edition):

Viswanath, Kamal. “Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat.” 2013. Doctoral Dissertation, Virginia Tech. Accessed January 26, 2021. http://hdl.handle.net/10919/50825.

MLA Handbook (7th Edition):

Viswanath, Kamal. “Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat.” 2013. Web. 26 Jan 2021.

Vancouver:

Viswanath K. Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/10919/50825.

Council of Science Editors:

Viswanath K. Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/50825


Cape Peninsula University of Technology

11. Zhou, Yan. Development of a data collection system for small Unmanned Aerial Vehicles (UAVs) .

Degree: 2011, Cape Peninsula University of Technology

 This paper presents the development of a data collection system for a small unmanned Aerial Vehicle (UAV) flight. The following three facets comprise of a… (more)

Subjects/Keywords: Drone aircraft; Vehicles, Remotely piloted; Automatic control; Flight control; Unmanned Aerial Vehicles; Dissertations, Academic; MTech; Theses, dissertations, etc.

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

APA (6th Edition):

Zhou, Y. (2011). Development of a data collection system for small Unmanned Aerial Vehicles (UAVs) . (Thesis). Cape Peninsula University of Technology. Retrieved from http://etd.cput.ac.za/handle/20.500.11838/1299

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

Chicago Manual of Style (16th Edition):

Zhou, Yan. “Development of a data collection system for small Unmanned Aerial Vehicles (UAVs) .” 2011. Thesis, Cape Peninsula University of Technology. Accessed January 26, 2021. http://etd.cput.ac.za/handle/20.500.11838/1299.

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

MLA Handbook (7th Edition):

Zhou, Yan. “Development of a data collection system for small Unmanned Aerial Vehicles (UAVs) .” 2011. Web. 26 Jan 2021.

Vancouver:

Zhou Y. Development of a data collection system for small Unmanned Aerial Vehicles (UAVs) . [Internet] [Thesis]. Cape Peninsula University of Technology; 2011. [cited 2021 Jan 26]. Available from: http://etd.cput.ac.za/handle/20.500.11838/1299.

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

Council of Science Editors:

Zhou Y. Development of a data collection system for small Unmanned Aerial Vehicles (UAVs) . [Thesis]. Cape Peninsula University of Technology; 2011. Available from: http://etd.cput.ac.za/handle/20.500.11838/1299

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


Ryerson University

12. Godard. Fault Tolerant Control Of Spacecraft.

Degree: 2010, Ryerson University

 Autonomous multiple spacecraft formation flying missions demand the development of reliable control systems to ensure rapid, accurate, and effective response to various attitude and formation… (more)

Subjects/Keywords: Fault tolerance (Engineering); Space flight  – Mathematical models; Space vehicles  – Attitude control systems; Space vehicles  – Control systems

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

APA (6th Edition):

Godard. (2010). Fault Tolerant Control Of Spacecraft. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1518

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

Chicago Manual of Style (16th Edition):

Godard. “Fault Tolerant Control Of Spacecraft.” 2010. Thesis, Ryerson University. Accessed January 26, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A1518.

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

MLA Handbook (7th Edition):

Godard. “Fault Tolerant Control Of Spacecraft.” 2010. Web. 26 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

Godard. Fault Tolerant Control Of Spacecraft. [Internet] [Thesis]. Ryerson University; 2010. [cited 2021 Jan 26]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1518.

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

Council of Science Editors:

Godard. Fault Tolerant Control Of Spacecraft. [Thesis]. Ryerson University; 2010. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1518

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


Delft University of Technology

13. Kelbling, Jelle (author). Trajectory control and dynamic modeling of a tailless flapping-wing robot.

Degree: 2020, Delft University of Technology

 The DelFly Nimble is a type of tailless flapping-wing micro air vehicles (FWMAVs) that has received an increasing amount of attention. FWMAVs show efficient and… (more)

Subjects/Keywords: Autonomous vehicles; Nonlinear control systems; Lie algebra; Flapping flight; Flapping wings; Micro air vehicles; Robotics; Trajectory tracking; Geometric Control

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

APA (6th Edition):

Kelbling, J. (. (2020). Trajectory control and dynamic modeling of a tailless flapping-wing robot. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b164a5d7-92c6-47d0-8fa0-5f3667b6d012

Chicago Manual of Style (16th Edition):

Kelbling, Jelle (author). “Trajectory control and dynamic modeling of a tailless flapping-wing robot.” 2020. Masters Thesis, Delft University of Technology. Accessed January 26, 2021. http://resolver.tudelft.nl/uuid:b164a5d7-92c6-47d0-8fa0-5f3667b6d012.

MLA Handbook (7th Edition):

Kelbling, Jelle (author). “Trajectory control and dynamic modeling of a tailless flapping-wing robot.” 2020. Web. 26 Jan 2021.

Vancouver:

Kelbling J(. Trajectory control and dynamic modeling of a tailless flapping-wing robot. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Jan 26]. Available from: http://resolver.tudelft.nl/uuid:b164a5d7-92c6-47d0-8fa0-5f3667b6d012.

Council of Science Editors:

Kelbling J(. Trajectory control and dynamic modeling of a tailless flapping-wing robot. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:b164a5d7-92c6-47d0-8fa0-5f3667b6d012


Indian Institute of Science

14. Mukherjee, Sujoy. Structural Modeling And Analysis Of Insect Scale Flapping Wing.

Degree: PhD, Faculty of Engineering, 2013, Indian Institute of Science

 Micro Air Vehicles (MAVs) are defined as a class of vehicles with their larger dimension not exceeding 15 cm and weighing 100 gm. The three… (more)

Subjects/Keywords: Flapping Wing; Micro Air Vehicles (MAVs); Calliphora Wing; Flapping Wings; Twisting Wing; Flapping Flight; Aeronautics

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

APA (6th Edition):

Mukherjee, S. (2013). Structural Modeling And Analysis Of Insect Scale Flapping Wing. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2021

Chicago Manual of Style (16th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2013. Doctoral Dissertation, Indian Institute of Science. Accessed January 26, 2021. http://etd.iisc.ac.in/handle/2005/2021.

MLA Handbook (7th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2013. Web. 26 Jan 2021.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2013. [cited 2021 Jan 26]. Available from: http://etd.iisc.ac.in/handle/2005/2021.

Council of Science Editors:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Doctoral Dissertation]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ac.in/handle/2005/2021


Delft University of Technology

15. Ketelaars, Martijn (author). Reduced-order modelling for prediction of aircraft flight dynamics: Based on indicial step response functions investigating agile aircraft undergoing rapid manoeuvres.

Degree: 2017, Delft University of Technology

 During aircraft design,multiple tools are utilised to inspect the performance of the configuration. As the design matures, higher fidelity analyses are conducted to predict the… (more)

Subjects/Keywords: Reduced order model; Flight dynamics; Surrogate modelling; Unmanned Aerial Vehicles; CFD; Modelling

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APA (6th Edition):

Ketelaars, M. (. (2017). Reduced-order modelling for prediction of aircraft flight dynamics: Based on indicial step response functions investigating agile aircraft undergoing rapid manoeuvres. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:244669d3-f4be-4df8-baa5-dca9ba9fc323

Chicago Manual of Style (16th Edition):

Ketelaars, Martijn (author). “Reduced-order modelling for prediction of aircraft flight dynamics: Based on indicial step response functions investigating agile aircraft undergoing rapid manoeuvres.” 2017. Masters Thesis, Delft University of Technology. Accessed January 26, 2021. http://resolver.tudelft.nl/uuid:244669d3-f4be-4df8-baa5-dca9ba9fc323.

MLA Handbook (7th Edition):

Ketelaars, Martijn (author). “Reduced-order modelling for prediction of aircraft flight dynamics: Based on indicial step response functions investigating agile aircraft undergoing rapid manoeuvres.” 2017. Web. 26 Jan 2021.

Vancouver:

Ketelaars M(. Reduced-order modelling for prediction of aircraft flight dynamics: Based on indicial step response functions investigating agile aircraft undergoing rapid manoeuvres. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 26]. Available from: http://resolver.tudelft.nl/uuid:244669d3-f4be-4df8-baa5-dca9ba9fc323.

Council of Science Editors:

Ketelaars M(. Reduced-order modelling for prediction of aircraft flight dynamics: Based on indicial step response functions investigating agile aircraft undergoing rapid manoeuvres. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:244669d3-f4be-4df8-baa5-dca9ba9fc323


Deakin University

16. Norton, Michael. Adaptive robust control of 6-DOF autonomous aerial vehicles.

Degree: 2015, Deakin University

 The thesis focused on development of an auto-pilot system for UAV’s and small fixed wing aircraft for use in hazardous flight conditions, such as severe… (more)

Subjects/Keywords: unmanned aerial vehicles; small fixed wing aircraft; auto-pilot system; hazardous flight conditions; 6-DOF

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APA (6th Edition):

Norton, M. (2015). Adaptive robust control of 6-DOF autonomous aerial vehicles. (Thesis). Deakin University. Retrieved from http://hdl.handle.net/10536/DRO/DU:30079382

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

Chicago Manual of Style (16th Edition):

Norton, Michael. “Adaptive robust control of 6-DOF autonomous aerial vehicles.” 2015. Thesis, Deakin University. Accessed January 26, 2021. http://hdl.handle.net/10536/DRO/DU:30079382.

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

MLA Handbook (7th Edition):

Norton, Michael. “Adaptive robust control of 6-DOF autonomous aerial vehicles.” 2015. Web. 26 Jan 2021.

Vancouver:

Norton M. Adaptive robust control of 6-DOF autonomous aerial vehicles. [Internet] [Thesis]. Deakin University; 2015. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/10536/DRO/DU:30079382.

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

Council of Science Editors:

Norton M. Adaptive robust control of 6-DOF autonomous aerial vehicles. [Thesis]. Deakin University; 2015. Available from: http://hdl.handle.net/10536/DRO/DU:30079382

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


University of Tennessee – Knoxville

17. Oegema, Kristopher Nathaniel. Design, Testing, and Calibration of a Custom Air Data Boom to Obtain Flight Data For the UTSI Cessna-T210J (N33UT).

Degree: MS, Engineering Science, 2015, University of Tennessee – Knoxville

Flight testing is dependent on the ability to accurately calculate the flight characteristics of an aircraft during a test. Any error caused by an… (more)

Subjects/Keywords: flight test; air data boom; airspeed; altitude; alpha; beta; Aeronautical Vehicles; Structures and Materials

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APA (6th Edition):

Oegema, K. N. (2015). Design, Testing, and Calibration of a Custom Air Data Boom to Obtain Flight Data For the UTSI Cessna-T210J (N33UT). (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/3397

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

Chicago Manual of Style (16th Edition):

Oegema, Kristopher Nathaniel. “Design, Testing, and Calibration of a Custom Air Data Boom to Obtain Flight Data For the UTSI Cessna-T210J (N33UT).” 2015. Thesis, University of Tennessee – Knoxville. Accessed January 26, 2021. https://trace.tennessee.edu/utk_gradthes/3397.

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

MLA Handbook (7th Edition):

Oegema, Kristopher Nathaniel. “Design, Testing, and Calibration of a Custom Air Data Boom to Obtain Flight Data For the UTSI Cessna-T210J (N33UT).” 2015. Web. 26 Jan 2021.

Vancouver:

Oegema KN. Design, Testing, and Calibration of a Custom Air Data Boom to Obtain Flight Data For the UTSI Cessna-T210J (N33UT). [Internet] [Thesis]. University of Tennessee – Knoxville; 2015. [cited 2021 Jan 26]. Available from: https://trace.tennessee.edu/utk_gradthes/3397.

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

Council of Science Editors:

Oegema KN. Design, Testing, and Calibration of a Custom Air Data Boom to Obtain Flight Data For the UTSI Cessna-T210J (N33UT). [Thesis]. University of Tennessee – Knoxville; 2015. Available from: https://trace.tennessee.edu/utk_gradthes/3397

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


University of New South Wales

18. Rehman, Obaid Ur. Robust Nonlinear Control System Design for Hypersonic Flight Vehicles.

Degree: Engineering & Information Technology, 2011, University of New South Wales

 This thesis develops a new nonlinear robust control design procedure which addresses some of the challenges associated with the control of uncertain nonlinear system and… (more)

Subjects/Keywords: Uncertain nonlinear system; Hypersonic flight vehicles; Robust nonlinear control system design; Feedback linerization

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APA (6th Edition):

Rehman, O. U. (2011). Robust Nonlinear Control System Design for Hypersonic Flight Vehicles. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/52045 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10715/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Rehman, Obaid Ur. “Robust Nonlinear Control System Design for Hypersonic Flight Vehicles.” 2011. Doctoral Dissertation, University of New South Wales. Accessed January 26, 2021. http://handle.unsw.edu.au/1959.4/52045 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10715/SOURCE01?view=true.

MLA Handbook (7th Edition):

Rehman, Obaid Ur. “Robust Nonlinear Control System Design for Hypersonic Flight Vehicles.” 2011. Web. 26 Jan 2021.

Vancouver:

Rehman OU. Robust Nonlinear Control System Design for Hypersonic Flight Vehicles. [Internet] [Doctoral dissertation]. University of New South Wales; 2011. [cited 2021 Jan 26]. Available from: http://handle.unsw.edu.au/1959.4/52045 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10715/SOURCE01?view=true.

Council of Science Editors:

Rehman OU. Robust Nonlinear Control System Design for Hypersonic Flight Vehicles. [Doctoral Dissertation]. University of New South Wales; 2011. Available from: http://handle.unsw.edu.au/1959.4/52045 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10715/SOURCE01?view=true


University of New South Wales

19. Yang, Xilin. Automatic Landing of a Rotary-Wing UAV in Rough Seas.

Degree: Engineering & Information Technology, 2011, University of New South Wales

 Rotary-wing unmanned aerial vehicles (RUAVs) have created extensive interest in the past few decades due to their unique manoeuverability and because of their suitability in… (more)

Subjects/Keywords: Automatic shipboard landings : simulations; Rotary-wing unmanned aerial vehicles (RUAVs); Flight control systems; Vario helicopters

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APA (6th Edition):

Yang, X. (2011). Automatic Landing of a Rotary-Wing UAV in Rough Seas. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/51446 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10132/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Yang, Xilin. “Automatic Landing of a Rotary-Wing UAV in Rough Seas.” 2011. Doctoral Dissertation, University of New South Wales. Accessed January 26, 2021. http://handle.unsw.edu.au/1959.4/51446 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10132/SOURCE01?view=true.

MLA Handbook (7th Edition):

Yang, Xilin. “Automatic Landing of a Rotary-Wing UAV in Rough Seas.” 2011. Web. 26 Jan 2021.

Vancouver:

Yang X. Automatic Landing of a Rotary-Wing UAV in Rough Seas. [Internet] [Doctoral dissertation]. University of New South Wales; 2011. [cited 2021 Jan 26]. Available from: http://handle.unsw.edu.au/1959.4/51446 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10132/SOURCE01?view=true.

Council of Science Editors:

Yang X. Automatic Landing of a Rotary-Wing UAV in Rough Seas. [Doctoral Dissertation]. University of New South Wales; 2011. Available from: http://handle.unsw.edu.au/1959.4/51446 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10132/SOURCE01?view=true


Ohio University

20. Bevacqua, Timothy R. Advanced Flight Control Issues for Reusable Launch Vehicles.

Degree: MS, Electrical Engineering & Computer Science (Engineering and Technology), 2004, Ohio University

  This thesis presents a flight control approach for reusable launch vehicles (RLVs). A detailed background of aerospace vehicle dynamics and control theory is provided,… (more)

Subjects/Keywords: Flight Control; Controls; Reusable Launch Vehicles

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APA (6th Edition):

Bevacqua, T. R. (2004). Advanced Flight Control Issues for Reusable Launch Vehicles. (Masters Thesis). Ohio University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1097601560

Chicago Manual of Style (16th Edition):

Bevacqua, Timothy R. “Advanced Flight Control Issues for Reusable Launch Vehicles.” 2004. Masters Thesis, Ohio University. Accessed January 26, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1097601560.

MLA Handbook (7th Edition):

Bevacqua, Timothy R. “Advanced Flight Control Issues for Reusable Launch Vehicles.” 2004. Web. 26 Jan 2021.

Vancouver:

Bevacqua TR. Advanced Flight Control Issues for Reusable Launch Vehicles. [Internet] [Masters thesis]. Ohio University; 2004. [cited 2021 Jan 26]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1097601560.

Council of Science Editors:

Bevacqua TR. Advanced Flight Control Issues for Reusable Launch Vehicles. [Masters Thesis]. Ohio University; 2004. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1097601560


University of Florida

21. GRZYWNA, JASON WESLEY ( Author, Primary ). A Flight Testbed with Virtual Environment Capabilities for Developing Autonomous Micro Air Vehicles.

Degree: University of Florida

Subjects/Keywords: Aircraft; Aircraft pitch; Aircraft roll; Earth stations; Environment simulation; Flight tests; Flight vehicles; Remotely piloted vehicles; Sensors; Vehicular flight

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APA (6th Edition):

GRZYWNA, JASON WESLEY ( Author, P. ). (n.d.). A Flight Testbed with Virtual Environment Capabilities for Developing Autonomous Micro Air Vehicles. (Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0008441

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

GRZYWNA, JASON WESLEY ( Author, Primary ). “A Flight Testbed with Virtual Environment Capabilities for Developing Autonomous Micro Air Vehicles.” Thesis, University of Florida. Accessed January 26, 2021. https://ufdc.ufl.edu/UFE0008441.

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

GRZYWNA, JASON WESLEY ( Author, Primary ). “A Flight Testbed with Virtual Environment Capabilities for Developing Autonomous Micro Air Vehicles.” Web. 26 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

GRZYWNA, JASON WESLEY ( Author P). A Flight Testbed with Virtual Environment Capabilities for Developing Autonomous Micro Air Vehicles. [Internet] [Thesis]. University of Florida; [cited 2021 Jan 26]. Available from: https://ufdc.ufl.edu/UFE0008441.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.

Council of Science Editors:

GRZYWNA, JASON WESLEY ( Author P). A Flight Testbed with Virtual Environment Capabilities for Developing Autonomous Micro Air Vehicles. [Thesis]. University of Florida; Available from: https://ufdc.ufl.edu/UFE0008441

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.


Indian Institute of Science

22. Das, Priya G. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.

Degree: PhD, Faculty of Engineering, 2011, Indian Institute of Science

 To address the concern of classical guidance and control designs (where guidance and control loops are designed separately in an “outer loop – inner loop”… (more)

Subjects/Keywords: Aerospace Vehicles - Guidance and Control; Interceptors (Aerospace Engineering); Guidance Systems (Flight); Flight Control; Endo-Atmospheric Interceptors; Partial Integrated Guidance and Control; Integrated Guidance and Control (IGC); Impact Angle Constraint; Astronautics

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APA (6th Edition):

Das, P. G. (2011). Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1099

Chicago Manual of Style (16th Edition):

Das, Priya G. “Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.” 2011. Doctoral Dissertation, Indian Institute of Science. Accessed January 26, 2021. http://etd.iisc.ac.in/handle/2005/1099.

MLA Handbook (7th Edition):

Das, Priya G. “Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.” 2011. Web. 26 Jan 2021.

Vancouver:

Das PG. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2011. [cited 2021 Jan 26]. Available from: http://etd.iisc.ac.in/handle/2005/1099.

Council of Science Editors:

Das PG. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. [Doctoral Dissertation]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ac.in/handle/2005/1099


University of Tennessee – Knoxville

23. Siu, Joe Ming Yin. Control Law Calculation and Verification Methods for the Variable Stability Navion In-Flight Simulation Aircraft.

Degree: MS, Aviation Systems, 2013, University of Tennessee – Knoxville

  The University of Tennessee Space Institute’s (UTSI) variable stability research aircraft, Ryan Navion N66UT, was extensively modified by the Princeton University in the 1960’s.… (more)

Subjects/Keywords: variable stability aircraft; Navion; in-flight simulation; flying quality; flight control law; model following; Aeronautical Vehicles; Controls and Control Theory; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Siu, J. M. Y. (2013). Control Law Calculation and Verification Methods for the Variable Stability Navion In-Flight Simulation Aircraft. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/1679

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

Chicago Manual of Style (16th Edition):

Siu, Joe Ming Yin. “Control Law Calculation and Verification Methods for the Variable Stability Navion In-Flight Simulation Aircraft.” 2013. Thesis, University of Tennessee – Knoxville. Accessed January 26, 2021. https://trace.tennessee.edu/utk_gradthes/1679.

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

MLA Handbook (7th Edition):

Siu, Joe Ming Yin. “Control Law Calculation and Verification Methods for the Variable Stability Navion In-Flight Simulation Aircraft.” 2013. Web. 26 Jan 2021.

Vancouver:

Siu JMY. Control Law Calculation and Verification Methods for the Variable Stability Navion In-Flight Simulation Aircraft. [Internet] [Thesis]. University of Tennessee – Knoxville; 2013. [cited 2021 Jan 26]. Available from: https://trace.tennessee.edu/utk_gradthes/1679.

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

Council of Science Editors:

Siu JMY. Control Law Calculation and Verification Methods for the Variable Stability Navion In-Flight Simulation Aircraft. [Thesis]. University of Tennessee – Knoxville; 2013. Available from: https://trace.tennessee.edu/utk_gradthes/1679

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


RMIT University

24. Khan, R. Fault tolerant flight control system design for unmanned aerial vehicles.

Degree: 2016, RMIT University

 Safety and reliability of air vehicles is of the utmost importance. This is particularly true for large civil transport aircraft where a large number of… (more)

Subjects/Keywords: Fields of Research; Unmanned aerial vehicles; Fault tolerant control; Model predictive control; Unscented Kalman filter; Flight control

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APA (6th Edition):

Khan, R. (2016). Fault tolerant flight control system design for unmanned aerial vehicles. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:161725

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

Chicago Manual of Style (16th Edition):

Khan, R. “Fault tolerant flight control system design for unmanned aerial vehicles.” 2016. Thesis, RMIT University. Accessed January 26, 2021. http://researchbank.rmit.edu.au/view/rmit:161725.

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

MLA Handbook (7th Edition):

Khan, R. “Fault tolerant flight control system design for unmanned aerial vehicles.” 2016. Web. 26 Jan 2021.

Vancouver:

Khan R. Fault tolerant flight control system design for unmanned aerial vehicles. [Internet] [Thesis]. RMIT University; 2016. [cited 2021 Jan 26]. Available from: http://researchbank.rmit.edu.au/view/rmit:161725.

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

Council of Science Editors:

Khan R. Fault tolerant flight control system design for unmanned aerial vehicles. [Thesis]. RMIT University; 2016. Available from: http://researchbank.rmit.edu.au/view/rmit:161725

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


Cape Peninsula University of Technology

25. Masango, Thubalakhe Patrick. Condition monitoring of a wing structure for an unmanned aerial vehicle (UAV) .

Degree: 2015, Cape Peninsula University of Technology

 Currently non-destructive testing techniques for composite aircraft structures are disadvantaged when compared to online Structural Health Monitoring (SHM) systems that monitor the structure while in-service… (more)

Subjects/Keywords: Drone aircraft; Drone aircraft  – Design and construction; Structural analysis (Engineering); Structural health monitoring; Vehicles, Remotely piloted; Flight control

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APA (6th Edition):

Masango, T. P. (2015). Condition monitoring of a wing structure for an unmanned aerial vehicle (UAV) . (Thesis). Cape Peninsula University of Technology. Retrieved from http://etd.cput.ac.za/handle/20.500.11838/2384

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

Chicago Manual of Style (16th Edition):

Masango, Thubalakhe Patrick. “Condition monitoring of a wing structure for an unmanned aerial vehicle (UAV) .” 2015. Thesis, Cape Peninsula University of Technology. Accessed January 26, 2021. http://etd.cput.ac.za/handle/20.500.11838/2384.

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

MLA Handbook (7th Edition):

Masango, Thubalakhe Patrick. “Condition monitoring of a wing structure for an unmanned aerial vehicle (UAV) .” 2015. Web. 26 Jan 2021.

Vancouver:

Masango TP. Condition monitoring of a wing structure for an unmanned aerial vehicle (UAV) . [Internet] [Thesis]. Cape Peninsula University of Technology; 2015. [cited 2021 Jan 26]. Available from: http://etd.cput.ac.za/handle/20.500.11838/2384.

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

Council of Science Editors:

Masango TP. Condition monitoring of a wing structure for an unmanned aerial vehicle (UAV) . [Thesis]. Cape Peninsula University of Technology; 2015. Available from: http://etd.cput.ac.za/handle/20.500.11838/2384

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


Ryerson University

26. Muthusamy, Venkatesh. Fault Detection, Isolation And Prognosis For Control Moment Gyros Onboard Satellites.

Degree: 2017, Ryerson University

 Developing a Diagnosis, Prognosis and Health Monitoring (DPHM) framework for a small satellite is a challenging task due to the limited availability of onboard health… (more)

Subjects/Keywords: Structural health monitoring; Fault tolerance (Engineering); Flight control; Actuators; Artificial satellites  – Control systems; Space vehicles  – Control systems

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APA (6th Edition):

Muthusamy, V. (2017). Fault Detection, Isolation And Prognosis For Control Moment Gyros Onboard Satellites. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6853

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

Chicago Manual of Style (16th Edition):

Muthusamy, Venkatesh. “Fault Detection, Isolation And Prognosis For Control Moment Gyros Onboard Satellites.” 2017. Thesis, Ryerson University. Accessed January 26, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A6853.

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

MLA Handbook (7th Edition):

Muthusamy, Venkatesh. “Fault Detection, Isolation And Prognosis For Control Moment Gyros Onboard Satellites.” 2017. Web. 26 Jan 2021.

Vancouver:

Muthusamy V. Fault Detection, Isolation And Prognosis For Control Moment Gyros Onboard Satellites. [Internet] [Thesis]. Ryerson University; 2017. [cited 2021 Jan 26]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6853.

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

Council of Science Editors:

Muthusamy V. Fault Detection, Isolation And Prognosis For Control Moment Gyros Onboard Satellites. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6853

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


University of Michigan

27. Al-Hiddabi, Saif Abdullah. Position tracking and path following for flight vehicles using nonlinear control.

Degree: PhD, Applied Sciences, 2000, University of Michigan

 This dissertation contributes to the subject of position tracking and path following for nonlinear non-minimum phase flight vehicle models. We show that the non-minimum phase… (more)

Subjects/Keywords: Flight Vehicles; Nonlinear Control; Path Following; Position Tracking; Using

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APA (6th Edition):

Al-Hiddabi, S. A. (2000). Position tracking and path following for flight vehicles using nonlinear control. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/132294

Chicago Manual of Style (16th Edition):

Al-Hiddabi, Saif Abdullah. “Position tracking and path following for flight vehicles using nonlinear control.” 2000. Doctoral Dissertation, University of Michigan. Accessed January 26, 2021. http://hdl.handle.net/2027.42/132294.

MLA Handbook (7th Edition):

Al-Hiddabi, Saif Abdullah. “Position tracking and path following for flight vehicles using nonlinear control.” 2000. Web. 26 Jan 2021.

Vancouver:

Al-Hiddabi SA. Position tracking and path following for flight vehicles using nonlinear control. [Internet] [Doctoral dissertation]. University of Michigan; 2000. [cited 2021 Jan 26]. Available from: http://hdl.handle.net/2027.42/132294.

Council of Science Editors:

Al-Hiddabi SA. Position tracking and path following for flight vehicles using nonlinear control. [Doctoral Dissertation]. University of Michigan; 2000. Available from: http://hdl.handle.net/2027.42/132294


West Virginia University

28. Rice, Caleb M. Control Design and Performance Analysis for Autonomous Formation Flight Experiments.

Degree: MS, Mechanical and Aerospace Engineering, 2014, West Virginia University

  Autonomous Formation Flight is a key approach for reducing greenhouse gas emissions and managing traffic in future high density airspace. Unmanned Aerial Vehicles (UAV’s)… (more)

Subjects/Keywords: flight control; nonlinear control design; quadrotor; fixed wing; Phastball; Aeronautical Vehicles; Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Rice, C. M. (2014). Control Design and Performance Analysis for Autonomous Formation Flight Experiments. (Thesis). West Virginia University. Retrieved from https://doi.org/10.33915/etd.6495 ; https://researchrepository.wvu.edu/etd/6495

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

Chicago Manual of Style (16th Edition):

Rice, Caleb M. “Control Design and Performance Analysis for Autonomous Formation Flight Experiments.” 2014. Thesis, West Virginia University. Accessed January 26, 2021. https://doi.org/10.33915/etd.6495 ; https://researchrepository.wvu.edu/etd/6495.

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

MLA Handbook (7th Edition):

Rice, Caleb M. “Control Design and Performance Analysis for Autonomous Formation Flight Experiments.” 2014. Web. 26 Jan 2021.

Vancouver:

Rice CM. Control Design and Performance Analysis for Autonomous Formation Flight Experiments. [Internet] [Thesis]. West Virginia University; 2014. [cited 2021 Jan 26]. Available from: https://doi.org/10.33915/etd.6495 ; https://researchrepository.wvu.edu/etd/6495.

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

Council of Science Editors:

Rice CM. Control Design and Performance Analysis for Autonomous Formation Flight Experiments. [Thesis]. West Virginia University; 2014. Available from: https://doi.org/10.33915/etd.6495 ; https://researchrepository.wvu.edu/etd/6495

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


Brigham Young University

29. Naegle, Nathaniel Stephen. Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism.

Degree: MS, 2012, Brigham Young University

  Flapping flight shows promise for micro air vehicle design because flapping wings provide superior aerodynamic performance than that of fixed wings and rotors at… (more)

Subjects/Keywords: flapping flight; flapping mechanism; water tunnel; hawkmoth; Box-Behnken; particle image velocimetry; PIV; flow characterization; micro-air vehicles; MAV; Mechanical Engineering

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

APA (6th Edition):

Naegle, N. S. (2012). Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd

Chicago Manual of Style (16th Edition):

Naegle, Nathaniel Stephen. “Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism.” 2012. Masters Thesis, Brigham Young University. Accessed January 26, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd.

MLA Handbook (7th Edition):

Naegle, Nathaniel Stephen. “Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism.” 2012. Web. 26 Jan 2021.

Vancouver:

Naegle NS. Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism. [Internet] [Masters thesis]. Brigham Young University; 2012. [cited 2021 Jan 26]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd.

Council of Science Editors:

Naegle NS. Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism. [Masters Thesis]. Brigham Young University; 2012. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd


University of Colorado

30. Baresi, Nicola. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.

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

  Since the successful rendezvous of the Gemini VI and VII spacecraft in 1965, spacecraft formation flying has attracted the interest of many researchers in… (more)

Subjects/Keywords: Astrodynamics; Cluster Flight; Dynamical Systems Theory; Quasi-periodic Invariant Tori; Spacecraft Formation Flying; Aerospace Engineering; Space Vehicles

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

APA (6th Edition):

Baresi, N. (2017). Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/176

Chicago Manual of Style (16th Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Doctoral Dissertation, University of Colorado. Accessed January 26, 2021. https://scholar.colorado.edu/asen_gradetds/176.

MLA Handbook (7th Edition):

Baresi, Nicola. “Spacecraft Formation Flight on Quasi-Periodic Invariant Tori.” 2017. Web. 26 Jan 2021.

Vancouver:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Jan 26]. Available from: https://scholar.colorado.edu/asen_gradetds/176.

Council of Science Editors:

Baresi N. Spacecraft Formation Flight on Quasi-Periodic Invariant Tori. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/176

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