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You searched for subject:(flight control). Showing records 1 – 30 of 470 total matches.

[1] [2] [3] [4] [5] … [16]

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Mississippi State University

1. Germann, Kenneth Paul. T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN.

Degree: PhD, Aerospace Engineering, 2009, Mississippi State University

 In-flight variable stability aircraft and in-flight simulation are described. The uses of these vehicles and the associated requirements are described. Several forms of control architecture… (more)

Subjects/Keywords: control; simulation; flight

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APA (6th Edition):

Germann, K. P. (2009). T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN. (Doctoral Dissertation). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-12162009-091123/ ;

Chicago Manual of Style (16th Edition):

Germann, Kenneth Paul. “T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN.” 2009. Doctoral Dissertation, Mississippi State University. Accessed September 19, 2020. http://sun.library.msstate.edu/ETD-db/theses/available/etd-12162009-091123/ ;.

MLA Handbook (7th Edition):

Germann, Kenneth Paul. “T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN.” 2009. Web. 19 Sep 2020.

Vancouver:

Germann KP. T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN. [Internet] [Doctoral dissertation]. Mississippi State University; 2009. [cited 2020 Sep 19]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-12162009-091123/ ;.

Council of Science Editors:

Germann KP. T-6A TEXAN II IN-FLIGHT SIMULATION AND VARIABLE STABILITY SYSTEM DESIGN. [Doctoral Dissertation]. Mississippi State University; 2009. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-12162009-091123/ ;


Oregon State University

2. Ray, Cody W. Modeling, control, and estimation of flexible, aerodynamic structures.

Degree: PhD, Mechanical Engineering, 2012, Oregon State University

 Engineers have long been inspired by nature's flyers. Such animals navigate complex environments gracefully and efficiently by using a variety of evolutionary adaptations for high-performance… (more)

Subjects/Keywords: Optimal control; Flight control

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APA (6th Edition):

Ray, C. W. (2012). Modeling, control, and estimation of flexible, aerodynamic structures. (Doctoral Dissertation). Oregon State University. Retrieved from http://hdl.handle.net/1957/29477

Chicago Manual of Style (16th Edition):

Ray, Cody W. “Modeling, control, and estimation of flexible, aerodynamic structures.” 2012. Doctoral Dissertation, Oregon State University. Accessed September 19, 2020. http://hdl.handle.net/1957/29477.

MLA Handbook (7th Edition):

Ray, Cody W. “Modeling, control, and estimation of flexible, aerodynamic structures.” 2012. Web. 19 Sep 2020.

Vancouver:

Ray CW. Modeling, control, and estimation of flexible, aerodynamic structures. [Internet] [Doctoral dissertation]. Oregon State University; 2012. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/1957/29477.

Council of Science Editors:

Ray CW. Modeling, control, and estimation of flexible, aerodynamic structures. [Doctoral Dissertation]. Oregon State University; 2012. Available from: http://hdl.handle.net/1957/29477


Brunel University

3. Bromfield, Michael. Criteria for acceptable stick force gradients of a light aeroplane.

Degree: PhD, 2012, Brunel University

 During the period 1980 to 2008 there were 359 fatal accidents involving UK registered light aeroplanes of which 36% occurred in visual meteorological conditions. In… (more)

Subjects/Keywords: 363.12; Flight safety; Control feel; Pilot workload; Flight simulation; Flight test

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APA (6th Edition):

Bromfield, M. (2012). Criteria for acceptable stick force gradients of a light aeroplane. (Doctoral Dissertation). Brunel University. Retrieved from http://bura.brunel.ac.uk/handle/2438/6861 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557870

Chicago Manual of Style (16th Edition):

Bromfield, Michael. “Criteria for acceptable stick force gradients of a light aeroplane.” 2012. Doctoral Dissertation, Brunel University. Accessed September 19, 2020. http://bura.brunel.ac.uk/handle/2438/6861 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557870.

MLA Handbook (7th Edition):

Bromfield, Michael. “Criteria for acceptable stick force gradients of a light aeroplane.” 2012. Web. 19 Sep 2020.

Vancouver:

Bromfield M. Criteria for acceptable stick force gradients of a light aeroplane. [Internet] [Doctoral dissertation]. Brunel University; 2012. [cited 2020 Sep 19]. Available from: http://bura.brunel.ac.uk/handle/2438/6861 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557870.

Council of Science Editors:

Bromfield M. Criteria for acceptable stick force gradients of a light aeroplane. [Doctoral Dissertation]. Brunel University; 2012. Available from: http://bura.brunel.ac.uk/handle/2438/6861 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.557870


Texas A&M University

4. Harris, Joshua A. Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems.

Degree: MS, Aerospace Engineering, 2017, Texas A&M University

 In-flight simulation and variable stability aircraft provide useful capabilities for flight controls development such as testing control laws for new aircraft earlier, identification of adverse… (more)

Subjects/Keywords: adaptive control; dynamic inversion; flight control; in-flight simulation

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APA (6th Edition):

Harris, J. A. (2017). Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/169626

Chicago Manual of Style (16th Edition):

Harris, Joshua A. “Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems.” 2017. Masters Thesis, Texas A&M University. Accessed September 19, 2020. http://hdl.handle.net/1969.1/169626.

MLA Handbook (7th Edition):

Harris, Joshua A. “Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems.” 2017. Web. 19 Sep 2020.

Vancouver:

Harris JA. Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems. [Internet] [Masters thesis]. Texas A&M University; 2017. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/1969.1/169626.

Council of Science Editors:

Harris JA. Nonlinear Adaptive Dynamic Inversion Control for Variable Stability Small Unmanned Aircraft Systems. [Masters Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/169626


Cape Peninsula University of Technology

5. Petersen, Michael. Development of a seamless morphing wing .

Degree: 2010, Cape Peninsula University of Technology

 The Cape Peninsula University of Technology (CPUT) Advanced Manufacturing and Technology Laboratory (AMTL) developed an Unmanned Aerial Vehicle (UAV) Technology Demonstrator for the purpose of… (more)

Subjects/Keywords: Morphing; Drone aircraft  – Control systems; Flight simulators; Flight control

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APA (6th Edition):

Petersen, M. (2010). Development of a seamless morphing wing . (Thesis). Cape Peninsula University of Technology. Retrieved from http://etd.cput.ac.za/handle/20.500.11838/2230

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):

Petersen, Michael. “Development of a seamless morphing wing .” 2010. Thesis, Cape Peninsula University of Technology. Accessed September 19, 2020. http://etd.cput.ac.za/handle/20.500.11838/2230.

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

MLA Handbook (7th Edition):

Petersen, Michael. “Development of a seamless morphing wing .” 2010. Web. 19 Sep 2020.

Vancouver:

Petersen M. Development of a seamless morphing wing . [Internet] [Thesis]. Cape Peninsula University of Technology; 2010. [cited 2020 Sep 19]. Available from: http://etd.cput.ac.za/handle/20.500.11838/2230.

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

Council of Science Editors:

Petersen M. Development of a seamless morphing wing . [Thesis]. Cape Peninsula University of Technology; 2010. Available from: http://etd.cput.ac.za/handle/20.500.11838/2230

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


University of Illinois – Urbana-Champaign

6. Paranjape, Aditya. Dynamics and control of robotic aircraft with articulated wings.

Degree: PhD, 4048, 2012, University of Illinois – Urbana-Champaign

 There is a considerable interest in developing robotic aircraft, inspired by birds, for a variety of missions covering reconnaissance and surveillance. Flapping wing aircraft concepts… (more)

Subjects/Keywords: Flight control; flight mechanics; PDE control; partial differential equation (PDE)

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APA (6th Edition):

Paranjape, A. (2012). Dynamics and control of robotic aircraft with articulated wings. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/29818

Chicago Manual of Style (16th Edition):

Paranjape, Aditya. “Dynamics and control of robotic aircraft with articulated wings.” 2012. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed September 19, 2020. http://hdl.handle.net/2142/29818.

MLA Handbook (7th Edition):

Paranjape, Aditya. “Dynamics and control of robotic aircraft with articulated wings.” 2012. Web. 19 Sep 2020.

Vancouver:

Paranjape A. Dynamics and control of robotic aircraft with articulated wings. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2012. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/2142/29818.

Council of Science Editors:

Paranjape A. Dynamics and control of robotic aircraft with articulated wings. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/29818


Virginia Tech

7. Shukla, Poorva Jahnukumar. Active Flight Path Control for an Induced Spin Flight Termination System.

Degree: MS, Engineering Mechanics, 2017, Virginia Tech

 In this thesis, we describe a method for controlling the cycle-averaged velocity direction of a fixed-wing aircraft in an unpowered, helical descent. While the aircraft… (more)

Subjects/Keywords: Linear Control Theory; Aerodynamic Flight Termination; Active Flight Path Control

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APA (6th Edition):

Shukla, P. J. (2017). Active Flight Path Control for an Induced Spin Flight Termination System. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78881

Chicago Manual of Style (16th Edition):

Shukla, Poorva Jahnukumar. “Active Flight Path Control for an Induced Spin Flight Termination System.” 2017. Masters Thesis, Virginia Tech. Accessed September 19, 2020. http://hdl.handle.net/10919/78881.

MLA Handbook (7th Edition):

Shukla, Poorva Jahnukumar. “Active Flight Path Control for an Induced Spin Flight Termination System.” 2017. Web. 19 Sep 2020.

Vancouver:

Shukla PJ. Active Flight Path Control for an Induced Spin Flight Termination System. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/10919/78881.

Council of Science Editors:

Shukla PJ. Active Flight Path Control for an Induced Spin Flight Termination System. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/78881


KTH

8. Knöös, Johan. Control of a Reusable Launch Vehicle.

Degree: Mathematics (Dept.), 2011, KTH

  Abstrakt: This report examines different control design methods, linear as well as nonlinear, for a suborbital reusable launch vehicle. An investigation of the natural… (more)

Subjects/Keywords: Flight control systems; nonlinear control; global optimization

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APA (6th Edition):

Knöös, J. (2011). Control of a Reusable Launch Vehicle. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-43837

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):

Knöös, Johan. “Control of a Reusable Launch Vehicle.” 2011. Thesis, KTH. Accessed September 19, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-43837.

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

MLA Handbook (7th Edition):

Knöös, Johan. “Control of a Reusable Launch Vehicle.” 2011. Web. 19 Sep 2020.

Vancouver:

Knöös J. Control of a Reusable Launch Vehicle. [Internet] [Thesis]. KTH; 2011. [cited 2020 Sep 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-43837.

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

Council of Science Editors:

Knöös J. Control of a Reusable Launch Vehicle. [Thesis]. KTH; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-43837

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


University of Southern California

9. Gadient, Ross. Adaptive control with aerospace applications.

Degree: PhD, Electrical Engineering, 2013, University of Southern California

 Robust and adaptive control techniques have a rich history of theoretical development with successful application. Despite the accomplishments made, attempts to combine the best elements… (more)

Subjects/Keywords: adaptive control; flight control; modern control; optimal control; robust control

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APA (6th Edition):

Gadient, R. (2013). Adaptive control with aerospace applications. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/225560/rec/512

Chicago Manual of Style (16th Edition):

Gadient, Ross. “Adaptive control with aerospace applications.” 2013. Doctoral Dissertation, University of Southern California. Accessed September 19, 2020. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/225560/rec/512.

MLA Handbook (7th Edition):

Gadient, Ross. “Adaptive control with aerospace applications.” 2013. Web. 19 Sep 2020.

Vancouver:

Gadient R. Adaptive control with aerospace applications. [Internet] [Doctoral dissertation]. University of Southern California; 2013. [cited 2020 Sep 19]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/225560/rec/512.

Council of Science Editors:

Gadient R. Adaptive control with aerospace applications. [Doctoral Dissertation]. University of Southern California; 2013. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/225560/rec/512


Ryerson University

10. 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 (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 September 19, 2020. 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. 19 Sep 2020.

Vancouver:

Li J. Intelligent Control of Satellite Formation Flying. [Internet] [Thesis]. Ryerson University; 2012. [cited 2020 Sep 19]. 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


Penn State University

11. Saetti, Umberto. Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads.

Degree: 2019, Penn State University

 The objective of this research effort is to develop rotorcraft flight control laws that minimize unsteady rotor loads by acting solely through the primary flight(more)

Subjects/Keywords: rotorcraft; flight controls; flight dynamics and control; flight dynamics; simulation; aerospace; aircraft; rotorcraft control; aircraft control; load alleviation; automatica flight control system; AFCS; control systems

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APA (6th Edition):

Saetti, U. (2019). Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/16696uxs116

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):

Saetti, Umberto. “Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads.” 2019. Thesis, Penn State University. Accessed September 19, 2020. https://submit-etda.libraries.psu.edu/catalog/16696uxs116.

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

MLA Handbook (7th Edition):

Saetti, Umberto. “Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads.” 2019. Web. 19 Sep 2020.

Vancouver:

Saetti U. Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads. [Internet] [Thesis]. Penn State University; 2019. [cited 2020 Sep 19]. Available from: https://submit-etda.libraries.psu.edu/catalog/16696uxs116.

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

Council of Science Editors:

Saetti U. Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads. [Thesis]. Penn State University; 2019. Available from: https://submit-etda.libraries.psu.edu/catalog/16696uxs116

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


Ryerson University

12. Sotto, Aaron. Using Presagis simulation software to model UAV aircraft in a humanitarian mission configuration.

Degree: 2016, Ryerson University

 Aircraft simulation software was used together to simulate a humanitarian variant of the MQ-9 Reaper drone as well as its longitudinal stability response upon dropping… (more)

Subjects/Keywords: Airplanes  – Performance; Airplanes  – Design and construction; Flight control; Aerodynamics; Flight simulators

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APA (6th Edition):

Sotto, A. (2016). Using Presagis simulation software to model UAV aircraft in a humanitarian mission configuration. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A5063

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):

Sotto, Aaron. “Using Presagis simulation software to model UAV aircraft in a humanitarian mission configuration.” 2016. Thesis, Ryerson University. Accessed September 19, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A5063.

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

MLA Handbook (7th Edition):

Sotto, Aaron. “Using Presagis simulation software to model UAV aircraft in a humanitarian mission configuration.” 2016. Web. 19 Sep 2020.

Vancouver:

Sotto A. Using Presagis simulation software to model UAV aircraft in a humanitarian mission configuration. [Internet] [Thesis]. Ryerson University; 2016. [cited 2020 Sep 19]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A5063.

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

Council of Science Editors:

Sotto A. Using Presagis simulation software to model UAV aircraft in a humanitarian mission configuration. [Thesis]. Ryerson University; 2016. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A5063

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


Virginia Tech

13. Ouellette, Jeffrey Alan. Modeling and Scaling of a Flexible Subscale Aircraft for Flight Control Development and Testing in the Presence of Aeroservoelastic Interactions.

Degree: PhD, Aerospace and Ocean Engineering, 2013, Virginia Tech

 The interaction of an aircraft's structure and the flight dynamics can degrade the performance of a controller designed only considering the rigid body flight dynamics.… (more)

Subjects/Keywords: Flight Dynamics; Flexible Structures; Aeroelasticity; Aeroservoelasticity; Subscale; Aircraft Scaling; Flight Control

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APA (6th Edition):

Ouellette, J. A. (2013). Modeling and Scaling of a Flexible Subscale Aircraft for Flight Control Development and Testing in the Presence of Aeroservoelastic Interactions. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/51819

Chicago Manual of Style (16th Edition):

Ouellette, Jeffrey Alan. “Modeling and Scaling of a Flexible Subscale Aircraft for Flight Control Development and Testing in the Presence of Aeroservoelastic Interactions.” 2013. Doctoral Dissertation, Virginia Tech. Accessed September 19, 2020. http://hdl.handle.net/10919/51819.

MLA Handbook (7th Edition):

Ouellette, Jeffrey Alan. “Modeling and Scaling of a Flexible Subscale Aircraft for Flight Control Development and Testing in the Presence of Aeroservoelastic Interactions.” 2013. Web. 19 Sep 2020.

Vancouver:

Ouellette JA. Modeling and Scaling of a Flexible Subscale Aircraft for Flight Control Development and Testing in the Presence of Aeroservoelastic Interactions. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/10919/51819.

Council of Science Editors:

Ouellette JA. Modeling and Scaling of a Flexible Subscale Aircraft for Flight Control Development and Testing in the Presence of Aeroservoelastic Interactions. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/51819


University of Washington

14. Dickerson, Bradley Horatio. The role of wing mechanosensory feedback in insect flight control.

Degree: PhD, 2015, University of Washington

 Flying insects rapidly stabilize after perturbations using multiple sensory modalities (e.g., vision mechanoreception, olfaction) for active control. Mechanoreceptors’ direct coupling of sensory structure to the… (more)

Subjects/Keywords: campaniform sensilla; flight control; Insect flight; Sensorimotor processing; Physiology; Neurosciences; biology

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APA (6th Edition):

Dickerson, B. H. (2015). The role of wing mechanosensory feedback in insect flight control. (Doctoral Dissertation). University of Washington. Retrieved from http://hdl.handle.net/1773/33603

Chicago Manual of Style (16th Edition):

Dickerson, Bradley Horatio. “The role of wing mechanosensory feedback in insect flight control.” 2015. Doctoral Dissertation, University of Washington. Accessed September 19, 2020. http://hdl.handle.net/1773/33603.

MLA Handbook (7th Edition):

Dickerson, Bradley Horatio. “The role of wing mechanosensory feedback in insect flight control.” 2015. Web. 19 Sep 2020.

Vancouver:

Dickerson BH. The role of wing mechanosensory feedback in insect flight control. [Internet] [Doctoral dissertation]. University of Washington; 2015. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/1773/33603.

Council of Science Editors:

Dickerson BH. The role of wing mechanosensory feedback in insect flight control. [Doctoral Dissertation]. University of Washington; 2015. Available from: http://hdl.handle.net/1773/33603


Delft University of Technology

15. Tal, E.A. (author). Coupled Flight Dynamic and Unsteady Aeroservoelastic Modeling and Control of a Flexible Wing Aircraft.

Degree: 2015, Delft University of Technology

Recent developments in airframe design include the increasing application of modern lightweight materials. Airframe designs based on composite materials are able to provide sufficient structural… (more)

Subjects/Keywords: flight dynamics; aeroelasticity; aeroservoelasticity; unsteady aerodynamics; flight control; vcctef

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APA (6th Edition):

Tal, E. A. (. (2015). Coupled Flight Dynamic and Unsteady Aeroservoelastic Modeling and Control of a Flexible Wing Aircraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5ba6ede0-6000-47ce-a229-2b65212a162f

Chicago Manual of Style (16th Edition):

Tal, E A (author). “Coupled Flight Dynamic and Unsteady Aeroservoelastic Modeling and Control of a Flexible Wing Aircraft.” 2015. Masters Thesis, Delft University of Technology. Accessed September 19, 2020. http://resolver.tudelft.nl/uuid:5ba6ede0-6000-47ce-a229-2b65212a162f.

MLA Handbook (7th Edition):

Tal, E A (author). “Coupled Flight Dynamic and Unsteady Aeroservoelastic Modeling and Control of a Flexible Wing Aircraft.” 2015. Web. 19 Sep 2020.

Vancouver:

Tal EA(. Coupled Flight Dynamic and Unsteady Aeroservoelastic Modeling and Control of a Flexible Wing Aircraft. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Sep 19]. Available from: http://resolver.tudelft.nl/uuid:5ba6ede0-6000-47ce-a229-2b65212a162f.

Council of Science Editors:

Tal EA(. Coupled Flight Dynamic and Unsteady Aeroservoelastic Modeling and Control of a Flexible Wing Aircraft. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:5ba6ede0-6000-47ce-a229-2b65212a162f


Delft University of Technology

16. Windels, E.R.G. (author). Formation Flight: Analysis of wake sensitivity, drag and control in trimmed flight.

Degree: 2015, Delft University of Technology

A research simulation model was created to perform extended research into formation flight dynamic behaviour. The principle of aircraft flying in formation is to lower… (more)

Subjects/Keywords: formation flight; formation flight trim; induced drag saving; formation flight stability; wake vortex field; A330-300; fuel saving; formation flight control

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APA (6th Edition):

Windels, E. R. G. (. (2015). Formation Flight: Analysis of wake sensitivity, drag and control in trimmed flight. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a65726f9-a873-442e-a186-b27202d9519a

Chicago Manual of Style (16th Edition):

Windels, E R G (author). “Formation Flight: Analysis of wake sensitivity, drag and control in trimmed flight.” 2015. Masters Thesis, Delft University of Technology. Accessed September 19, 2020. http://resolver.tudelft.nl/uuid:a65726f9-a873-442e-a186-b27202d9519a.

MLA Handbook (7th Edition):

Windels, E R G (author). “Formation Flight: Analysis of wake sensitivity, drag and control in trimmed flight.” 2015. Web. 19 Sep 2020.

Vancouver:

Windels ERG(. Formation Flight: Analysis of wake sensitivity, drag and control in trimmed flight. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Sep 19]. Available from: http://resolver.tudelft.nl/uuid:a65726f9-a873-442e-a186-b27202d9519a.

Council of Science Editors:

Windels ERG(. Formation Flight: Analysis of wake sensitivity, drag and control in trimmed flight. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:a65726f9-a873-442e-a186-b27202d9519a


Univerzitet u Beogradu

17. Stojaković, Predrag V. Анализа утицаја спољашњих терета и асиметричних оптерећења на динамику лета авиона.

Degree: Mašinski fakultet, 2013, Univerzitet u Beogradu

Ваздухопловство - Динамика и управљање летом авиона / Aeronautics - Airplane dynamics and flight control

номинална, ограничена на основни облик авиона са геометријском и инерцијалном… (more)

Subjects/Keywords: Airplane flight dynamics; Flight mechanics; Flight control system design; Airplane flying qualities; Mathematical modeling of airplane flight dynamics; External stores; Airplane asymmetric loads; Flight controls; Flight envelope boundaries

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APA (6th Edition):

Stojaković, P. V. (2013). Анализа утицаја спољашњих терета и асиметричних оптерећења на динамику лета авиона. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:6025/bdef:Content/get

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):

Stojaković, Predrag V. “Анализа утицаја спољашњих терета и асиметричних оптерећења на динамику лета авиона.” 2013. Thesis, Univerzitet u Beogradu. Accessed September 19, 2020. https://fedorabg.bg.ac.rs/fedora/get/o:6025/bdef:Content/get.

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

MLA Handbook (7th Edition):

Stojaković, Predrag V. “Анализа утицаја спољашњих терета и асиметричних оптерећења на динамику лета авиона.” 2013. Web. 19 Sep 2020.

Vancouver:

Stojaković PV. Анализа утицаја спољашњих терета и асиметричних оптерећења на динамику лета авиона. [Internet] [Thesis]. Univerzitet u Beogradu; 2013. [cited 2020 Sep 19]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:6025/bdef:Content/get.

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

Council of Science Editors:

Stojaković PV. Анализа утицаја спољашњих терета и асиметричних оптерећења на динамику лета авиона. [Thesis]. Univerzitet u Beogradu; 2013. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:6025/bdef:Content/get

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


Cornell University

18. Ristroph, Leif. Dynamics, Control, And Stability Of Fruit Fly Flight.

Degree: PhD, Physics, 2011, Cornell University

 The flight of insects is a beautiful example of an organism's complex interaction with its physical environment. Consider, for example, a fly's evasive dodge of… (more)

Subjects/Keywords: Insect flight; Aerodynamics; Stability and control

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APA (6th Edition):

Ristroph, L. (2011). Dynamics, Control, And Stability Of Fruit Fly Flight. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/29392

Chicago Manual of Style (16th Edition):

Ristroph, Leif. “Dynamics, Control, And Stability Of Fruit Fly Flight.” 2011. Doctoral Dissertation, Cornell University. Accessed September 19, 2020. http://hdl.handle.net/1813/29392.

MLA Handbook (7th Edition):

Ristroph, Leif. “Dynamics, Control, And Stability Of Fruit Fly Flight.” 2011. Web. 19 Sep 2020.

Vancouver:

Ristroph L. Dynamics, Control, And Stability Of Fruit Fly Flight. [Internet] [Doctoral dissertation]. Cornell University; 2011. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/1813/29392.

Council of Science Editors:

Ristroph L. Dynamics, Control, And Stability Of Fruit Fly Flight. [Doctoral Dissertation]. Cornell University; 2011. Available from: http://hdl.handle.net/1813/29392


Anna University

19. Senthil kumar K. Design and development of terminal phase flight control system for an unmanned air vehicle;.

Degree: Design and development of terminal phase flight control system for an unmanned air vehicle, 2014, Anna University

The ultimate aim of both military and commercial aviation is allweather newlineoperation To achieve this goal it should be possible to land the newlineaircraft without… (more)

Subjects/Keywords: air vehicle; electrical engineering; flight control system

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APA (6th Edition):

K, S. k. (2014). Design and development of terminal phase flight control system for an unmanned air vehicle;. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/31658

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):

K, Senthil kumar. “Design and development of terminal phase flight control system for an unmanned air vehicle;.” 2014. Thesis, Anna University. Accessed September 19, 2020. http://shodhganga.inflibnet.ac.in/handle/10603/31658.

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

MLA Handbook (7th Edition):

K, Senthil kumar. “Design and development of terminal phase flight control system for an unmanned air vehicle;.” 2014. Web. 19 Sep 2020.

Vancouver:

K Sk. Design and development of terminal phase flight control system for an unmanned air vehicle;. [Internet] [Thesis]. Anna University; 2014. [cited 2020 Sep 19]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/31658.

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

Council of Science Editors:

K Sk. Design and development of terminal phase flight control system for an unmanned air vehicle;. [Thesis]. Anna University; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/31658

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


Stellenbosch University

20. Smit, Samuel Jacobus Adriaan. Autonomous landing of a fixed-wing unmanned aerial vehicle using differential GPS.

Degree: MScEng, Electrical and Electronic Engineering, 2013, Stellenbosch University

ENGLISH ABSTRACT: This dissertation presents the design and practical demonstration of a flight control system (FCS) that is capable of autonomously landing a fixed-wing, unmanned… (more)

Subjects/Keywords: Electronic engineering; Drone aircraft; Flight control

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APA (6th Edition):

Smit, S. J. A. (2013). Autonomous landing of a fixed-wing unmanned aerial vehicle using differential GPS. (Masters Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/80122

Chicago Manual of Style (16th Edition):

Smit, Samuel Jacobus Adriaan. “Autonomous landing of a fixed-wing unmanned aerial vehicle using differential GPS.” 2013. Masters Thesis, Stellenbosch University. Accessed September 19, 2020. http://hdl.handle.net/10019.1/80122.

MLA Handbook (7th Edition):

Smit, Samuel Jacobus Adriaan. “Autonomous landing of a fixed-wing unmanned aerial vehicle using differential GPS.” 2013. Web. 19 Sep 2020.

Vancouver:

Smit SJA. Autonomous landing of a fixed-wing unmanned aerial vehicle using differential GPS. [Internet] [Masters thesis]. Stellenbosch University; 2013. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/10019.1/80122.

Council of Science Editors:

Smit SJA. Autonomous landing of a fixed-wing unmanned aerial vehicle using differential GPS. [Masters Thesis]. Stellenbosch University; 2013. Available from: http://hdl.handle.net/10019.1/80122


Stellenbosch University

21. Basson, Lionel. Control allocation as part of a fault-tolerant control architecture for UAVs.

Degree: Electrical and Electronic Engineering, 2011, Stellenbosch University

Thesis (MScEng (Electrical and Electronic Engineering)) – University of Stellenbosch, 2011.

ENGLISH ABSTRACT: The development of a control allocation system for use as part of a… (more)

Subjects/Keywords: Electronic engineering; Drone aircraft; Flight control

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APA (6th Edition):

Basson, L. (2011). Control allocation as part of a fault-tolerant control architecture for UAVs. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/6722

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):

Basson, Lionel. “Control allocation as part of a fault-tolerant control architecture for UAVs.” 2011. Thesis, Stellenbosch University. Accessed September 19, 2020. http://hdl.handle.net/10019.1/6722.

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

MLA Handbook (7th Edition):

Basson, Lionel. “Control allocation as part of a fault-tolerant control architecture for UAVs.” 2011. Web. 19 Sep 2020.

Vancouver:

Basson L. Control allocation as part of a fault-tolerant control architecture for UAVs. [Internet] [Thesis]. Stellenbosch University; 2011. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/10019.1/6722.

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

Council of Science Editors:

Basson L. Control allocation as part of a fault-tolerant control architecture for UAVs. [Thesis]. Stellenbosch University; 2011. Available from: http://hdl.handle.net/10019.1/6722

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


Rochester Institute of Technology

22. Hussain, Heather. Verification and validation of a theoretical model of a direct drive valve-controlled electrohydrostatic actuator for primary flight control.

Degree: Mechanical Engineering, 2012, Rochester Institute of Technology

  In this work, a theoretical parametric nonlinear model for a hybrid variable pressure actuator was verified through dynamic system modeling techniques and validated using… (more)

Subjects/Keywords: Actuator; Electrohydrostatic; Flight Control; Hydraulic; Valve-Controlled

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APA (6th Edition):

Hussain, H. (2012). Verification and validation of a theoretical model of a direct drive valve-controlled electrohydrostatic actuator for primary flight control. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5806

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):

Hussain, Heather. “Verification and validation of a theoretical model of a direct drive valve-controlled electrohydrostatic actuator for primary flight control.” 2012. Thesis, Rochester Institute of Technology. Accessed September 19, 2020. https://scholarworks.rit.edu/theses/5806.

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

MLA Handbook (7th Edition):

Hussain, Heather. “Verification and validation of a theoretical model of a direct drive valve-controlled electrohydrostatic actuator for primary flight control.” 2012. Web. 19 Sep 2020.

Vancouver:

Hussain H. Verification and validation of a theoretical model of a direct drive valve-controlled electrohydrostatic actuator for primary flight control. [Internet] [Thesis]. Rochester Institute of Technology; 2012. [cited 2020 Sep 19]. Available from: https://scholarworks.rit.edu/theses/5806.

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

Council of Science Editors:

Hussain H. Verification and validation of a theoretical model of a direct drive valve-controlled electrohydrostatic actuator for primary flight control. [Thesis]. Rochester Institute of Technology; 2012. Available from: https://scholarworks.rit.edu/theses/5806

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

23. Balogh, Shelby. Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight.

Degree: MS, Aviation, 2017, University of North Dakota

  The leading cause of fatal aviation accidents worldwide remains loss of control in-flight, whereby control of the aircraft is lost or the aircraft enters… (more)

Subjects/Keywords: Aviation Safety; Loss of Control In-flight

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APA (6th Edition):

Balogh, S. (2017). Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/2099

Chicago Manual of Style (16th Edition):

Balogh, Shelby. “Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight.” 2017. Masters Thesis, University of North Dakota. Accessed September 19, 2020. https://commons.und.edu/theses/2099.

MLA Handbook (7th Edition):

Balogh, Shelby. “Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight.” 2017. Web. 19 Sep 2020.

Vancouver:

Balogh S. Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight. [Internet] [Masters thesis]. University of North Dakota; 2017. [cited 2020 Sep 19]. Available from: https://commons.und.edu/theses/2099.

Council of Science Editors:

Balogh S. Use Of FOQA Data To Estimate The Probability Of Vehicle Upset Or Loss Of Control In-Flight. [Masters Thesis]. University of North Dakota; 2017. Available from: https://commons.und.edu/theses/2099


Oregon State University

24. Ray, Cody W. Modeling and control of a biologically inspired compliant structure.

Degree: MS, Mechanical Engineering, 2009, Oregon State University

 We hypothesize that the extraordinary maneuverability and efficiency of bats in flight are in part due to the compliant nature of their wing structures. We… (more)

Subjects/Keywords: Optimal Control; Bats  – Flight  – Mathematical models

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APA (6th Edition):

Ray, C. W. (2009). Modeling and control of a biologically inspired compliant structure. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/11737

Chicago Manual of Style (16th Edition):

Ray, Cody W. “Modeling and control of a biologically inspired compliant structure.” 2009. Masters Thesis, Oregon State University. Accessed September 19, 2020. http://hdl.handle.net/1957/11737.

MLA Handbook (7th Edition):

Ray, Cody W. “Modeling and control of a biologically inspired compliant structure.” 2009. Web. 19 Sep 2020.

Vancouver:

Ray CW. Modeling and control of a biologically inspired compliant structure. [Internet] [Masters thesis]. Oregon State University; 2009. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/1957/11737.

Council of Science Editors:

Ray CW. Modeling and control of a biologically inspired compliant structure. [Masters Thesis]. Oregon State University; 2009. Available from: http://hdl.handle.net/1957/11737


Loughborough University

25. Smith, Jean. Design and application of advanced disturbance rejection control for small fixed-wing UAVs.

Degree: PhD, 2018, Loughborough University

 Small Unmanned Aerial Vehicles (UAVs) have seen continual growth in both research and commercial applications. Attractive features such as their small size, light weight and… (more)

Subjects/Keywords: 629.133; UAV; Flight control; Disturbance rejection; DOBC

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APA (6th Edition):

Smith, J. (2018). Design and application of advanced disturbance rejection control for small fixed-wing UAVs. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/33543

Chicago Manual of Style (16th Edition):

Smith, Jean. “Design and application of advanced disturbance rejection control for small fixed-wing UAVs.” 2018. Doctoral Dissertation, Loughborough University. Accessed September 19, 2020. http://hdl.handle.net/2134/33543.

MLA Handbook (7th Edition):

Smith, Jean. “Design and application of advanced disturbance rejection control for small fixed-wing UAVs.” 2018. Web. 19 Sep 2020.

Vancouver:

Smith J. Design and application of advanced disturbance rejection control for small fixed-wing UAVs. [Internet] [Doctoral dissertation]. Loughborough University; 2018. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/2134/33543.

Council of Science Editors:

Smith J. Design and application of advanced disturbance rejection control for small fixed-wing UAVs. [Doctoral Dissertation]. Loughborough University; 2018. Available from: http://hdl.handle.net/2134/33543


Delft University of Technology

26. Selvan, A. (author). Simulation of optic flow based flight control for a flapping wing micro aerial vehicle.

Degree: 2014, Delft University of Technology

Bio-inspired flying micro drones, formally known as Flapping Wing Micro Aerial Vehicles (FWMAV) are a booming class of robots in today's world. Navigation and flight(more)

Subjects/Keywords: FWMAV; MAV; Optic flow; Flight control

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APA (6th Edition):

Selvan, A. (. (2014). Simulation of optic flow based flight control for a flapping wing micro aerial vehicle. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3

Chicago Manual of Style (16th Edition):

Selvan, A (author). “Simulation of optic flow based flight control for a flapping wing micro aerial vehicle.” 2014. Masters Thesis, Delft University of Technology. Accessed September 19, 2020. http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3.

MLA Handbook (7th Edition):

Selvan, A (author). “Simulation of optic flow based flight control for a flapping wing micro aerial vehicle.” 2014. Web. 19 Sep 2020.

Vancouver:

Selvan A(. Simulation of optic flow based flight control for a flapping wing micro aerial vehicle. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2020 Sep 19]. Available from: http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3.

Council of Science Editors:

Selvan A(. Simulation of optic flow based flight control for a flapping wing micro aerial vehicle. [Masters Thesis]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3


University of Victoria

27. Zhang, Kunwu. Flight control of a quadrotor: theory and experiments.

Degree: Department of Mechanical Engineering, 2016, University of Victoria

 In the last decades, the quadrotor has been used in many areas, and deigning an effective flight control algorithm for the quadrotor has attracted great… (more)

Subjects/Keywords: Quadrotor; Flight control; EKF; LQR; MPC

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APA (6th Edition):

Zhang, K. (2016). Flight control of a quadrotor: theory and experiments. (Masters Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/7426

Chicago Manual of Style (16th Edition):

Zhang, Kunwu. “Flight control of a quadrotor: theory and experiments.” 2016. Masters Thesis, University of Victoria. Accessed September 19, 2020. http://hdl.handle.net/1828/7426.

MLA Handbook (7th Edition):

Zhang, Kunwu. “Flight control of a quadrotor: theory and experiments.” 2016. Web. 19 Sep 2020.

Vancouver:

Zhang K. Flight control of a quadrotor: theory and experiments. [Internet] [Masters thesis]. University of Victoria; 2016. [cited 2020 Sep 19]. Available from: http://hdl.handle.net/1828/7426.

Council of Science Editors:

Zhang K. Flight control of a quadrotor: theory and experiments. [Masters Thesis]. University of Victoria; 2016. Available from: http://hdl.handle.net/1828/7426


Ryerson University

28. 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 September 19, 2020. 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. 19 Sep 2020.

Vancouver:

Lin AKL. Control of spacecraft formation flying around asteroids. [Internet] [Thesis]. Ryerson University; 2014. [cited 2020 Sep 19]. 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


Cranfield University

29. Lone, M. Mudassir. Pilot modelling for airframe loads analysis.

Degree: PhD, 2013, Cranfield University

 The development of large lightweight airframes has resulted in what used to be high frequency structural dynamics entering the low frequency range associated with an… (more)

Subjects/Keywords: Pilot modelling; manual control; pilot-model-in-the-loop simulation; flight loads; aeroelastics; flight control

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APA (6th Edition):

Lone, M. M. (2013). Pilot modelling for airframe loads analysis. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10388

Chicago Manual of Style (16th Edition):

Lone, M Mudassir. “Pilot modelling for airframe loads analysis.” 2013. Doctoral Dissertation, Cranfield University. Accessed September 19, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/10388.

MLA Handbook (7th Edition):

Lone, M Mudassir. “Pilot modelling for airframe loads analysis.” 2013. Web. 19 Sep 2020.

Vancouver:

Lone MM. Pilot modelling for airframe loads analysis. [Internet] [Doctoral dissertation]. Cranfield University; 2013. [cited 2020 Sep 19]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10388.

Council of Science Editors:

Lone MM. Pilot modelling for airframe loads analysis. [Doctoral Dissertation]. Cranfield University; 2013. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10388


University of North Texas

30. AL-Emrani, Firas. A Preliminary Controller Design for Drone Carried Directional Communication System.

Degree: 2015, University of North Texas

 In this thesis, we conduct a preliminary study on the controller design for directional antenna devices carried by drones. The goal of the control system… (more)

Subjects/Keywords: Control system design; Drone aircraft  – Control systems.; Flight control.; Antennas (Electronics)

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APA (6th Edition):

AL-Emrani, F. (2015). A Preliminary Controller Design for Drone Carried Directional Communication System. (Thesis). University of North Texas. Retrieved from https://digital.library.unt.edu/ark:/67531/metadc804990/

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):

AL-Emrani, Firas. “A Preliminary Controller Design for Drone Carried Directional Communication System.” 2015. Thesis, University of North Texas. Accessed September 19, 2020. https://digital.library.unt.edu/ark:/67531/metadc804990/.

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

MLA Handbook (7th Edition):

AL-Emrani, Firas. “A Preliminary Controller Design for Drone Carried Directional Communication System.” 2015. Web. 19 Sep 2020.

Vancouver:

AL-Emrani F. A Preliminary Controller Design for Drone Carried Directional Communication System. [Internet] [Thesis]. University of North Texas; 2015. [cited 2020 Sep 19]. Available from: https://digital.library.unt.edu/ark:/67531/metadc804990/.

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

Council of Science Editors:

AL-Emrani F. A Preliminary Controller Design for Drone Carried Directional Communication System. [Thesis]. University of North Texas; 2015. Available from: https://digital.library.unt.edu/ark:/67531/metadc804990/

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

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