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You searched for +publisher:"Delft University of Technology" +contributor:("Chu, Q.P."). Showing records 1 – 23 of 23 total matches.

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Delft University of Technology

1. Fragoso Trigo, G. (author). Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs.

Degree: 2011, Delft University of Technology

 <p>In the context of the initiative Formation for Atmospheric Science and Technology demonstration (FAST), this dissertation describes the design and comparison of several nonlinear attitude… (more)

Subjects/Keywords: Spacecraft Attitude Control; Robust Control; Adaptive Control; Backstepping; Immersion and Invariance; Modified Rodrigues Parameters

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APA (6th Edition):

Fragoso Trigo, G. (. (2011). Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce

Chicago Manual of Style (16th Edition):

Fragoso Trigo, G (author). “Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs.” 2011. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce.

MLA Handbook (7th Edition):

Fragoso Trigo, G (author). “Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs.” 2011. Web. 22 Sep 2020.

Vancouver:

Fragoso Trigo G(. Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce.

Council of Science Editors:

Fragoso Trigo G(. Robust and Adaptive Nonlinear Attitude Control of a Spacacraft: A Comparison of Backstepping-based Designs. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:ac9a05df-7c33-4dae-9d34-5e667e6168ce


Delft University of Technology

2. Van Gils, P. (author). Adaptive Incremental Backstepping Flight Control.

Degree: 2015, Delft University of Technology

 <p>This thesis deals with the development of Adaptive Incremental Backstepping control laws for a high-performance aircraft model (F-16), in order to make the airplane robustly… (more)

Subjects/Keywords: flight control; incremental control; robust control; adaptive control; fault-tolerant; backstepping; adaptive backstepping; incremental backstepping; parameter estimation; system identification; immersion and invariance; tuning functions; recursive least-squares

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APA (6th Edition):

Van Gils, P. (. (2015). Adaptive Incremental Backstepping Flight Control. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f62ac38d-5101-4230-ad90-d54543c1f1b8

Chicago Manual of Style (16th Edition):

Van Gils, P (author). “Adaptive Incremental Backstepping Flight Control.” 2015. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:f62ac38d-5101-4230-ad90-d54543c1f1b8.

MLA Handbook (7th Edition):

Van Gils, P (author). “Adaptive Incremental Backstepping Flight Control.” 2015. Web. 22 Sep 2020.

Vancouver:

Van Gils P(. Adaptive Incremental Backstepping Flight Control. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:f62ac38d-5101-4230-ad90-d54543c1f1b8.

Council of Science Editors:

Van Gils P(. Adaptive Incremental Backstepping Flight Control. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:f62ac38d-5101-4230-ad90-d54543c1f1b8


Delft University of Technology

3. Simplicio, P. (author). Helicopter nonlinear flight control: An acceleration measurements-based approach using incremental nonlinear dynamic inversion.

Degree: 2011, Delft University of Technology

 <p>Due to the inherent instabilities and nonlinearities of rotorcraft dynamics, its changing properties during flight and the difficulties to predict its aerodynamics with high levels… (more)

Subjects/Keywords: helicopter modeling; helicopter flight control; nonlinear dynamic inversion; incremental nonlinear dynamic inversion; pseudo-control hedging

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APA (6th Edition):

Simplicio, P. (. (2011). Helicopter nonlinear flight control: An acceleration measurements-based approach using incremental nonlinear dynamic inversion. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d2ffe4d1-219e-4965-a6b4-debb900ded4c

Chicago Manual of Style (16th Edition):

Simplicio, P (author). “Helicopter nonlinear flight control: An acceleration measurements-based approach using incremental nonlinear dynamic inversion.” 2011. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:d2ffe4d1-219e-4965-a6b4-debb900ded4c.

MLA Handbook (7th Edition):

Simplicio, P (author). “Helicopter nonlinear flight control: An acceleration measurements-based approach using incremental nonlinear dynamic inversion.” 2011. Web. 22 Sep 2020.

Vancouver:

Simplicio P(. Helicopter nonlinear flight control: An acceleration measurements-based approach using incremental nonlinear dynamic inversion. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:d2ffe4d1-219e-4965-a6b4-debb900ded4c.

Council of Science Editors:

Simplicio P(. Helicopter nonlinear flight control: An acceleration measurements-based approach using incremental nonlinear dynamic inversion. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:d2ffe4d1-219e-4965-a6b4-debb900ded4c


Delft University of Technology

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

Degree: 2015, Delft University of Technology

 <p>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 22, 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. 22 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 22]. 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

5. van 't Veld, R.C. (author). Incremental Nonlinear Dynamic Inversion Flight Control: Stability and Robustness Analysis and Improvements.

Degree: 2016, Delft University of Technology

 <p>Incremental Nonlinear Dynamic Inversion (INDI) is a variation on Nonlinear Dynamic Inversion (NDI) retaining the high-performance advantages of NDI, while increasing controller robustness to model… (more)

Subjects/Keywords: Incremental Nonlinear Dynamic Inversion; Aircraft Attitude Control; Stability; Robustness

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APA (6th Edition):

van 't Veld, R. C. (. (2016). Incremental Nonlinear Dynamic Inversion Flight Control: Stability and Robustness Analysis and Improvements. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f85a9c88-7bdb-42cd-a01c-aa85251d365c

Chicago Manual of Style (16th Edition):

van 't Veld, R C (author). “Incremental Nonlinear Dynamic Inversion Flight Control: Stability and Robustness Analysis and Improvements.” 2016. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:f85a9c88-7bdb-42cd-a01c-aa85251d365c.

MLA Handbook (7th Edition):

van 't Veld, R C (author). “Incremental Nonlinear Dynamic Inversion Flight Control: Stability and Robustness Analysis and Improvements.” 2016. Web. 22 Sep 2020.

Vancouver:

van 't Veld RC(. Incremental Nonlinear Dynamic Inversion Flight Control: Stability and Robustness Analysis and Improvements. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:f85a9c88-7bdb-42cd-a01c-aa85251d365c.

Council of Science Editors:

van 't Veld RC(. Incremental Nonlinear Dynamic Inversion Flight Control: Stability and Robustness Analysis and Improvements. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:f85a9c88-7bdb-42cd-a01c-aa85251d365c


Delft University of Technology

6. Van Baelen, D. (author). Evaluation of a non-linear control law for control loading devices.

Degree: 2016, Delft University of Technology

 <p>Simulator control loading systems are used to replicate the forces felt on the control devices. In the actual vehicle, the control system is a passive… (more)

Subjects/Keywords: control loading device; control loading system; cls; non-linear; control law; energy-based

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APA (6th Edition):

Van Baelen, D. (. (2016). Evaluation of a non-linear control law for control loading devices. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e0df2ee8-99ed-4117-8a47-ec264b9f2be3

Chicago Manual of Style (16th Edition):

Van Baelen, D (author). “Evaluation of a non-linear control law for control loading devices.” 2016. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:e0df2ee8-99ed-4117-8a47-ec264b9f2be3.

MLA Handbook (7th Edition):

Van Baelen, D (author). “Evaluation of a non-linear control law for control loading devices.” 2016. Web. 22 Sep 2020.

Vancouver:

Van Baelen D(. Evaluation of a non-linear control law for control loading devices. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:e0df2ee8-99ed-4117-8a47-ec264b9f2be3.

Council of Science Editors:

Van Baelen D(. Evaluation of a non-linear control law for control loading devices. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:e0df2ee8-99ed-4117-8a47-ec264b9f2be3


Delft University of Technology

7. Acquatella, B.P.J. (author). Robust Nonlinear Spacecraft Attitude Control: An Incremental Backstepping Approach.

Degree: 2011, Delft University of Technology

 <p>In order to meet requirements in terms of robustness, stability, and performance for future generations of advanced attitude control systems, a sensor-based approach using Incremental… (more)

Subjects/Keywords: Spacecraft Attitude Control; Nonlinear Control; Backstepping; Incremental Backstepping; Incremental Nonlinear Dynamic Inversion; Lyapunov-based control; Modified Rodrigues Parameters

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APA (6th Edition):

Acquatella, B. P. J. (. (2011). Robust Nonlinear Spacecraft Attitude Control: An Incremental Backstepping Approach. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a56090a3-bbce-404b-8e4b-d0e9050b518a

Chicago Manual of Style (16th Edition):

Acquatella, B P J (author). “Robust Nonlinear Spacecraft Attitude Control: An Incremental Backstepping Approach.” 2011. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:a56090a3-bbce-404b-8e4b-d0e9050b518a.

MLA Handbook (7th Edition):

Acquatella, B P J (author). “Robust Nonlinear Spacecraft Attitude Control: An Incremental Backstepping Approach.” 2011. Web. 22 Sep 2020.

Vancouver:

Acquatella BPJ(. Robust Nonlinear Spacecraft Attitude Control: An Incremental Backstepping Approach. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:a56090a3-bbce-404b-8e4b-d0e9050b518a.

Council of Science Editors:

Acquatella BPJ(. Robust Nonlinear Spacecraft Attitude Control: An Incremental Backstepping Approach. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:a56090a3-bbce-404b-8e4b-d0e9050b518a


Delft University of Technology

8. Ferrier, Y.L. (author). Active Gust Load Alleviation for Flexible Wing Aircraft.

Degree: 2017, Delft University of Technology

 <p>This paper presents a novel active gust load alleviation approach within a multi-objective flight control framework developed by NASA for a flexible wing aircraft. The… (more)

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APA (6th Edition):

Ferrier, Y. L. (. (2017). Active Gust Load Alleviation for Flexible Wing Aircraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8c3fccad-e708-48db-baaa-c99dbe496d21

Chicago Manual of Style (16th Edition):

Ferrier, Y L (author). “Active Gust Load Alleviation for Flexible Wing Aircraft.” 2017. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:8c3fccad-e708-48db-baaa-c99dbe496d21.

MLA Handbook (7th Edition):

Ferrier, Y L (author). “Active Gust Load Alleviation for Flexible Wing Aircraft.” 2017. Web. 22 Sep 2020.

Vancouver:

Ferrier YL(. Active Gust Load Alleviation for Flexible Wing Aircraft. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:8c3fccad-e708-48db-baaa-c99dbe496d21.

Council of Science Editors:

Ferrier YL(. Active Gust Load Alleviation for Flexible Wing Aircraft. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:8c3fccad-e708-48db-baaa-c99dbe496d21


Delft University of Technology

9. Koschorke, J.F.R. (author). Advanced Flight Control Design and Evaluation: An application of time delayed Incremental Backstepping.

Degree: 2012, Delft University of Technology

 <p>The sensor-based approach of Incremental Backstepping is applied to flight control law design in this research project. It allows the usage of the same control… (more)

Subjects/Keywords: Incremental Backstepping; Time delay; Lyapunov-based control; Fly-By-Wire; Diamond DA 42; Nonlinear; Sensor-based control; SAFAR; Pilot-in-the-loop; Aircraft rate control; Flight control evaluation; SSV

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APA (6th Edition):

Koschorke, J. F. R. (. (2012). Advanced Flight Control Design and Evaluation: An application of time delayed Incremental Backstepping. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:24c0bfab-3243-4ffa-9c96-10a4721fb23a

Chicago Manual of Style (16th Edition):

Koschorke, J F R (author). “Advanced Flight Control Design and Evaluation: An application of time delayed Incremental Backstepping.” 2012. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:24c0bfab-3243-4ffa-9c96-10a4721fb23a.

MLA Handbook (7th Edition):

Koschorke, J F R (author). “Advanced Flight Control Design and Evaluation: An application of time delayed Incremental Backstepping.” 2012. Web. 22 Sep 2020.

Vancouver:

Koschorke JFR(. Advanced Flight Control Design and Evaluation: An application of time delayed Incremental Backstepping. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:24c0bfab-3243-4ffa-9c96-10a4721fb23a.

Council of Science Editors:

Koschorke JFR(. Advanced Flight Control Design and Evaluation: An application of time delayed Incremental Backstepping. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:24c0bfab-3243-4ffa-9c96-10a4721fb23a


Delft University of Technology

10. Hummelink, B.A. (author). Fixed-Wing UAV Integrated Navigation with Low-Cost IMU/GPS.

Degree: 2011, Delft University of Technology

 Today, there is an increase in the use of Unmanned Aerial Vehicles (UAV's), for applications that can be considered dull, dirty or dangerous when compared… (more)

Subjects/Keywords: UAV; IMU; GPS; Kalman; filtering; identification; observability; Lie groups

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APA (6th Edition):

Hummelink, B. A. (. (2011). Fixed-Wing UAV Integrated Navigation with Low-Cost IMU/GPS. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:291207fc-5ada-435c-be39-8e1436fd96c9

Chicago Manual of Style (16th Edition):

Hummelink, B A (author). “Fixed-Wing UAV Integrated Navigation with Low-Cost IMU/GPS.” 2011. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:291207fc-5ada-435c-be39-8e1436fd96c9.

MLA Handbook (7th Edition):

Hummelink, B A (author). “Fixed-Wing UAV Integrated Navigation with Low-Cost IMU/GPS.” 2011. Web. 22 Sep 2020.

Vancouver:

Hummelink BA(. Fixed-Wing UAV Integrated Navigation with Low-Cost IMU/GPS. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:291207fc-5ada-435c-be39-8e1436fd96c9.

Council of Science Editors:

Hummelink BA(. Fixed-Wing UAV Integrated Navigation with Low-Cost IMU/GPS. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:291207fc-5ada-435c-be39-8e1436fd96c9


Delft University of Technology

11. Govindarajan, N. (author). An optimal control approach for estimating aircraft command margins.

Degree: 2012, Delft University of Technology

 <p>This dissertation presents an optimal control framework to determine a collection of open-loop command signals, that mathematically guarantees operation of a dynamical system within prescribed… (more)

Subjects/Keywords: optimal control; Hamilton Jacobi Bellman PDE; flight envelope protection; reachability

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APA (6th Edition):

Govindarajan, N. (. (2012). An optimal control approach for estimating aircraft command margins. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:48dbad61-728a-4c7e-ba3e-cf8382ef1cef

Chicago Manual of Style (16th Edition):

Govindarajan, N (author). “An optimal control approach for estimating aircraft command margins.” 2012. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:48dbad61-728a-4c7e-ba3e-cf8382ef1cef.

MLA Handbook (7th Edition):

Govindarajan, N (author). “An optimal control approach for estimating aircraft command margins.” 2012. Web. 22 Sep 2020.

Vancouver:

Govindarajan N(. An optimal control approach for estimating aircraft command margins. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:48dbad61-728a-4c7e-ba3e-cf8382ef1cef.

Council of Science Editors:

Govindarajan N(. An optimal control approach for estimating aircraft command margins. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:48dbad61-728a-4c7e-ba3e-cf8382ef1cef


Delft University of Technology

12. Tang, S.H. (author). Fault-Tolerant Flight Control with Sensor-Based Nonlinear Dynamic Inversion.

Degree: 2014, Delft University of Technology

 <p>A worldwide civil aviation accident survey for the period of 2002 till 2011, conducted by the CAA-UK shows that in this time period nearly 40%… (more)

Subjects/Keywords: fault-tolerant; flight control; piloted simulation; model-independent; backstepping; nonlinear dynamic inversion; NDI; sensor-based

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APA (6th Edition):

Tang, S. H. (. (2014). Fault-Tolerant Flight Control with Sensor-Based Nonlinear Dynamic Inversion. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c2263beb-602b-4727-9219-43cd11325622

Chicago Manual of Style (16th Edition):

Tang, S H (author). “Fault-Tolerant Flight Control with Sensor-Based Nonlinear Dynamic Inversion.” 2014. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:c2263beb-602b-4727-9219-43cd11325622.

MLA Handbook (7th Edition):

Tang, S H (author). “Fault-Tolerant Flight Control with Sensor-Based Nonlinear Dynamic Inversion.” 2014. Web. 22 Sep 2020.

Vancouver:

Tang SH(. Fault-Tolerant Flight Control with Sensor-Based Nonlinear Dynamic Inversion. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:c2263beb-602b-4727-9219-43cd11325622.

Council of Science Editors:

Tang SH(. Fault-Tolerant Flight Control with Sensor-Based Nonlinear Dynamic Inversion. [Masters Thesis]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:c2263beb-602b-4727-9219-43cd11325622


Delft University of Technology

13. Trullas Ballester, Marc (author). Asteroid Mission Guidance and Control using Dual Quaternions.

Degree: 2018, Delft University of Technology

 <p>The investigation of small bodies in the Solar System such as asteroids and comets is of increasing interest to the space exploration community for scientific… (more)

Subjects/Keywords: Asteroids; Dual Quaternions; Control; Attitude; Pose; Quaternions; Landing; Hover; Orbit

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APA (6th Edition):

Trullas Ballester, M. (. (2018). Asteroid Mission Guidance and Control using Dual Quaternions. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:49257a61-5d9e-402d-acde-e82ef5fa6ed8

Chicago Manual of Style (16th Edition):

Trullas Ballester, Marc (author). “Asteroid Mission Guidance and Control using Dual Quaternions.” 2018. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:49257a61-5d9e-402d-acde-e82ef5fa6ed8.

MLA Handbook (7th Edition):

Trullas Ballester, Marc (author). “Asteroid Mission Guidance and Control using Dual Quaternions.” 2018. Web. 22 Sep 2020.

Vancouver:

Trullas Ballester M(. Asteroid Mission Guidance and Control using Dual Quaternions. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:49257a61-5d9e-402d-acde-e82ef5fa6ed8.

Council of Science Editors:

Trullas Ballester M(. Asteroid Mission Guidance and Control using Dual Quaternions. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:49257a61-5d9e-402d-acde-e82ef5fa6ed8

14. Mendes, A.S. (author). Vision-based automatic landing of a quadrotor UAV on a floating platform: A new approach using incremental backstepping.

Degree: 2012, Delft University of Technology

 The development of systems that allow unmanned aerial vehicles, known as UAVs, to perform tasks autonomously is a current trend in aerospace research. The specific… (more)

Subjects/Keywords: Quadrotor UAV; Moments of inertia experiment; Computer vision; Augmented Kalman filtering; Incremental backstepping; Monte-Carlo simulations; Real-time implementation

…Transform Discrete-Time Fourier Transform Delft University of Technology Extended Kalman Filter… …Lab (MAVlab) at the Delft University of Technology (DUT) are taking this… …University of Technology February 2012 Alexandre Santos Mendes Vision-based automatic landing of a… …parents, my brother and Amber for always supporting and encouraging me in everything I do. Delft… 

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APA (6th Edition):

Mendes, A. S. (. (2012). Vision-based automatic landing of a quadrotor UAV on a floating platform: A new approach using incremental backstepping. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f8848255-1831-482a-be21-2da3ca3e50bb

Chicago Manual of Style (16th Edition):

Mendes, A S (author). “Vision-based automatic landing of a quadrotor UAV on a floating platform: A new approach using incremental backstepping.” 2012. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:f8848255-1831-482a-be21-2da3ca3e50bb.

MLA Handbook (7th Edition):

Mendes, A S (author). “Vision-based automatic landing of a quadrotor UAV on a floating platform: A new approach using incremental backstepping.” 2012. Web. 22 Sep 2020.

Vancouver:

Mendes AS(. Vision-based automatic landing of a quadrotor UAV on a floating platform: A new approach using incremental backstepping. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:f8848255-1831-482a-be21-2da3ca3e50bb.

Council of Science Editors:

Mendes AS(. Vision-based automatic landing of a quadrotor UAV on a floating platform: A new approach using incremental backstepping. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:f8848255-1831-482a-be21-2da3ca3e50bb


Delft University of Technology

15. Reijerkerk, M.J. Aeroelastic model identification of winglet loads from flight test data.

Degree: 2008, Delft University of Technology

 Numerical computational methods are getting more and more sophisticated every day, enabling more accurate aircraft load predictions. In the structural design of aircraft higher levels… (more)

Subjects/Keywords: flight test identification; flight loads analysis; winglets; wing tip devices; maximum likelihood; aeroelasticity; multi-disciplinary modelling

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APA (6th Edition):

Reijerkerk, M. J. (2008). Aeroelastic model identification of winglet loads from flight test data. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; urn:NBN:nl:ui:24-uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; urn:NBN:nl:ui:24-uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; http://resolver.tudelft.nl/uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1

Chicago Manual of Style (16th Edition):

Reijerkerk, M J. “Aeroelastic model identification of winglet loads from flight test data.” 2008. Doctoral Dissertation, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; urn:NBN:nl:ui:24-uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; urn:NBN:nl:ui:24-uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; http://resolver.tudelft.nl/uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1.

MLA Handbook (7th Edition):

Reijerkerk, M J. “Aeroelastic model identification of winglet loads from flight test data.” 2008. Web. 22 Sep 2020.

Vancouver:

Reijerkerk MJ. Aeroelastic model identification of winglet loads from flight test data. [Internet] [Doctoral dissertation]. Delft University of Technology; 2008. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; urn:NBN:nl:ui:24-uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; urn:NBN:nl:ui:24-uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; http://resolver.tudelft.nl/uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1.

Council of Science Editors:

Reijerkerk MJ. Aeroelastic model identification of winglet loads from flight test data. [Doctoral Dissertation]. Delft University of Technology; 2008. Available from: http://resolver.tudelft.nl/uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; urn:NBN:nl:ui:24-uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; urn:NBN:nl:ui:24-uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1 ; http://resolver.tudelft.nl/uuid:3b516cb3-33e6-433f-8cf3-bb0e9e9feae1


Delft University of Technology

16. Looye, G.H.N. An Integrated Approach to Aircraft Modelling and Flight Control Law Design.

Degree: 2008, Delft University of Technology

 The design of flight control laws (FCLs) for automatic and manual (augmented) control of aircraft is a complicated task. FCLs have to fulfil large amounts… (more)

Subjects/Keywords: flight dynamics; flight control; aeroelasticity; multi-disciplinary modelling; multi-objective optimisation

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APA (6th Edition):

Looye, G. H. N. (2008). An Integrated Approach to Aircraft Modelling and Flight Control Law Design. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; urn:NBN:nl:ui:24-uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; urn:NBN:nl:ui:24-uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; http://resolver.tudelft.nl/uuid:3c921dd4-c9f5-439e-a412-afd0856ba689

Chicago Manual of Style (16th Edition):

Looye, G H N. “An Integrated Approach to Aircraft Modelling and Flight Control Law Design.” 2008. Doctoral Dissertation, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; urn:NBN:nl:ui:24-uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; urn:NBN:nl:ui:24-uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; http://resolver.tudelft.nl/uuid:3c921dd4-c9f5-439e-a412-afd0856ba689.

MLA Handbook (7th Edition):

Looye, G H N. “An Integrated Approach to Aircraft Modelling and Flight Control Law Design.” 2008. Web. 22 Sep 2020.

Vancouver:

Looye GHN. An Integrated Approach to Aircraft Modelling and Flight Control Law Design. [Internet] [Doctoral dissertation]. Delft University of Technology; 2008. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; urn:NBN:nl:ui:24-uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; urn:NBN:nl:ui:24-uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; http://resolver.tudelft.nl/uuid:3c921dd4-c9f5-439e-a412-afd0856ba689.

Council of Science Editors:

Looye GHN. An Integrated Approach to Aircraft Modelling and Flight Control Law Design. [Doctoral Dissertation]. Delft University of Technology; 2008. Available from: http://resolver.tudelft.nl/uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; urn:NBN:nl:ui:24-uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; urn:NBN:nl:ui:24-uuid:3c921dd4-c9f5-439e-a412-afd0856ba689 ; http://resolver.tudelft.nl/uuid:3c921dd4-c9f5-439e-a412-afd0856ba689


Delft University of Technology

17. Van Oort, E.R. Adaptive Backstepping Control and Safety Analysis for Modern Fighter Aircraft.

Degree: 2011, Delft University of Technology

 There exist many examples of aircraft incidents in which the pilots have successfully used the remaining control authority over an aircraft to save the airframe… (more)

Subjects/Keywords: adaptive control; identification; aircraft; safety; nonlinear control; level set

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APA (6th Edition):

Van Oort, E. R. (2011). Adaptive Backstepping Control and Safety Analysis for Modern Fighter Aircraft. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; urn:NBN:nl:ui:24-uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; urn:NBN:nl:ui:24-uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; http://resolver.tudelft.nl/uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48

Chicago Manual of Style (16th Edition):

Van Oort, E R. “Adaptive Backstepping Control and Safety Analysis for Modern Fighter Aircraft.” 2011. Doctoral Dissertation, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; urn:NBN:nl:ui:24-uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; urn:NBN:nl:ui:24-uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; http://resolver.tudelft.nl/uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48.

MLA Handbook (7th Edition):

Van Oort, E R. “Adaptive Backstepping Control and Safety Analysis for Modern Fighter Aircraft.” 2011. Web. 22 Sep 2020.

Vancouver:

Van Oort ER. Adaptive Backstepping Control and Safety Analysis for Modern Fighter Aircraft. [Internet] [Doctoral dissertation]. Delft University of Technology; 2011. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; urn:NBN:nl:ui:24-uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; urn:NBN:nl:ui:24-uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; http://resolver.tudelft.nl/uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48.

Council of Science Editors:

Van Oort ER. Adaptive Backstepping Control and Safety Analysis for Modern Fighter Aircraft. [Doctoral Dissertation]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; urn:NBN:nl:ui:24-uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; urn:NBN:nl:ui:24-uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48 ; http://resolver.tudelft.nl/uuid:68fd89ff-aad6-4ad8-b280-d2fe8b500d48


Delft University of Technology

18. Sonneveldt, L. Adaptive Backstepping Flight Control for Modern Fighter Aircraft.

Degree: 2010, Delft University of Technology

 The main goal of this thesis is to investigate the potential of the nonlinear adaptive backstepping control technique in combination with online model identification for… (more)

Subjects/Keywords: flight control; adaptive control; system identification; backstepping; Lyapunov; nonlinear control

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APA (6th Edition):

Sonneveldt, L. (2010). Adaptive Backstepping Flight Control for Modern Fighter Aircraft. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; urn:NBN:nl:ui:24-uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; urn:NBN:nl:ui:24-uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; http://resolver.tudelft.nl/uuid:a21d2cc6-9924-4018-9387-60527fb27d4b

Chicago Manual of Style (16th Edition):

Sonneveldt, L. “Adaptive Backstepping Flight Control for Modern Fighter Aircraft.” 2010. Doctoral Dissertation, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; urn:NBN:nl:ui:24-uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; urn:NBN:nl:ui:24-uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; http://resolver.tudelft.nl/uuid:a21d2cc6-9924-4018-9387-60527fb27d4b.

MLA Handbook (7th Edition):

Sonneveldt, L. “Adaptive Backstepping Flight Control for Modern Fighter Aircraft.” 2010. Web. 22 Sep 2020.

Vancouver:

Sonneveldt L. Adaptive Backstepping Flight Control for Modern Fighter Aircraft. [Internet] [Doctoral dissertation]. Delft University of Technology; 2010. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; urn:NBN:nl:ui:24-uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; urn:NBN:nl:ui:24-uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; http://resolver.tudelft.nl/uuid:a21d2cc6-9924-4018-9387-60527fb27d4b.

Council of Science Editors:

Sonneveldt L. Adaptive Backstepping Flight Control for Modern Fighter Aircraft. [Doctoral Dissertation]. Delft University of Technology; 2010. Available from: http://resolver.tudelft.nl/uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; urn:NBN:nl:ui:24-uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; urn:NBN:nl:ui:24-uuid:a21d2cc6-9924-4018-9387-60527fb27d4b ; http://resolver.tudelft.nl/uuid:a21d2cc6-9924-4018-9387-60527fb27d4b


Delft University of Technology

19. Verveld, M.J. (author). Optical Flow Based State Estimation for an Indoor Micro Aerial Vehicle.

Degree: 2009, Delft University of Technology

 <p>This work addresses the problem of indoor state estimation for autonomous flying vehicles with an optic flow approach. The paper discusses a sensor configuration using… (more)

Subjects/Keywords: optical flow; sensor fusion; Unscented Kalman filter; bio-inspired flight

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APA (6th Edition):

Verveld, M. J. (. (2009). Optical Flow Based State Estimation for an Indoor Micro Aerial Vehicle. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:fe5ea73c-a85b-4a4b-b5d5-fc01d29b2113

Chicago Manual of Style (16th Edition):

Verveld, M J (author). “Optical Flow Based State Estimation for an Indoor Micro Aerial Vehicle.” 2009. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:fe5ea73c-a85b-4a4b-b5d5-fc01d29b2113.

MLA Handbook (7th Edition):

Verveld, M J (author). “Optical Flow Based State Estimation for an Indoor Micro Aerial Vehicle.” 2009. Web. 22 Sep 2020.

Vancouver:

Verveld MJ(. Optical Flow Based State Estimation for an Indoor Micro Aerial Vehicle. [Internet] [Masters thesis]. Delft University of Technology; 2009. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:fe5ea73c-a85b-4a4b-b5d5-fc01d29b2113.

Council of Science Editors:

Verveld MJ(. Optical Flow Based State Estimation for an Indoor Micro Aerial Vehicle. [Masters Thesis]. Delft University of Technology; 2009. Available from: http://resolver.tudelft.nl/uuid:fe5ea73c-a85b-4a4b-b5d5-fc01d29b2113


Delft University of Technology

20. Grotens, R. (author). Nonlinear Flight Control: Fault Tolerant Control with Sliding Modes and Control Allocation.

Degree: 2010, Delft University of Technology

 <p>Nonlinear Dynamic Inversion (NDI) is a promising method for Fault Tolerant Flight Control. The NDI algorithm cancels out the aircraft dynamics based on a dynamic… (more)

Subjects/Keywords: Fault Tolerant Flight Control; Nonlinear Dynamic Inversion; Sliding Mode Control; Control Allocation

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APA (6th Edition):

Grotens, R. (. (2010). Nonlinear Flight Control: Fault Tolerant Control with Sliding Modes and Control Allocation. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:29ddf25f-bcc3-47f3-9c26-53da9b6d9301

Chicago Manual of Style (16th Edition):

Grotens, R (author). “Nonlinear Flight Control: Fault Tolerant Control with Sliding Modes and Control Allocation.” 2010. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:29ddf25f-bcc3-47f3-9c26-53da9b6d9301.

MLA Handbook (7th Edition):

Grotens, R (author). “Nonlinear Flight Control: Fault Tolerant Control with Sliding Modes and Control Allocation.” 2010. Web. 22 Sep 2020.

Vancouver:

Grotens R(. Nonlinear Flight Control: Fault Tolerant Control with Sliding Modes and Control Allocation. [Internet] [Masters thesis]. Delft University of Technology; 2010. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:29ddf25f-bcc3-47f3-9c26-53da9b6d9301.

Council of Science Editors:

Grotens R(. Nonlinear Flight Control: Fault Tolerant Control with Sliding Modes and Control Allocation. [Masters Thesis]. Delft University of Technology; 2010. Available from: http://resolver.tudelft.nl/uuid:29ddf25f-bcc3-47f3-9c26-53da9b6d9301


Delft University of Technology

21. Kers, M. (author). Maximum Likelihood Estimation of Linear Time-Varying Pilot-Vehicle System Parameters.

Degree: 2012, Delft University of Technology

Human-Machine Interaction

Control & Operations

Aerospace Engineering

Advisors/Committee Members: Mulder, M. (mentor), Pool, D.M. (mentor), Van Paassen, M.M. (mentor), Chu, Q.P. (mentor).

Subjects/Keywords: Maximum Likelihood Estimation; Human-Machine Interaction; HMI; aerospace; system identification; parameter estimation; Gauss-Newton; Boltzmann Sigmoid; control; simulation; modeling; LTV; Linear Time-Varying; MLE

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APA (6th Edition):

Kers, M. (. (2012). Maximum Likelihood Estimation of Linear Time-Varying Pilot-Vehicle System Parameters. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f5819979-5874-497d-9ec5-8645916b9c9a

Chicago Manual of Style (16th Edition):

Kers, M (author). “Maximum Likelihood Estimation of Linear Time-Varying Pilot-Vehicle System Parameters.” 2012. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:f5819979-5874-497d-9ec5-8645916b9c9a.

MLA Handbook (7th Edition):

Kers, M (author). “Maximum Likelihood Estimation of Linear Time-Varying Pilot-Vehicle System Parameters.” 2012. Web. 22 Sep 2020.

Vancouver:

Kers M(. Maximum Likelihood Estimation of Linear Time-Varying Pilot-Vehicle System Parameters. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:f5819979-5874-497d-9ec5-8645916b9c9a.

Council of Science Editors:

Kers M(. Maximum Likelihood Estimation of Linear Time-Varying Pilot-Vehicle System Parameters. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:f5819979-5874-497d-9ec5-8645916b9c9a


Delft University of Technology

22. Filipe, N.R.S. (author). Terminal area energy management trajectory optimization using interval analysis.

Degree: Aerospace Engineering, Control and Simulation, 2008, Delft University of Technology

Aerospace Engineering Advisors/Committee Members: Mulder, J.A. (mentor), Chu, Q.P. (mentor), Barrio, A.M. (mentor), Van Kampen, E. (mentor), De Weerdt, E. (mentor), ESA/ESTEC (contributor).

Subjects/Keywords: trajectory optimization; interval analysis; taem; horus-2b; global optimization

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APA (6th Edition):

Filipe, N. R. S. (. (2008). Terminal area energy management trajectory optimization using interval analysis. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:38b137be-3afc-4fbb-a1ad-0fdb6eeb451e

Chicago Manual of Style (16th Edition):

Filipe, N R S (author). “Terminal area energy management trajectory optimization using interval analysis.” 2008. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:38b137be-3afc-4fbb-a1ad-0fdb6eeb451e.

MLA Handbook (7th Edition):

Filipe, N R S (author). “Terminal area energy management trajectory optimization using interval analysis.” 2008. Web. 22 Sep 2020.

Vancouver:

Filipe NRS(. Terminal area energy management trajectory optimization using interval analysis. [Internet] [Masters thesis]. Delft University of Technology; 2008. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:38b137be-3afc-4fbb-a1ad-0fdb6eeb451e.

Council of Science Editors:

Filipe NRS(. Terminal area energy management trajectory optimization using interval analysis. [Masters Thesis]. Delft University of Technology; 2008. Available from: http://resolver.tudelft.nl/uuid:38b137be-3afc-4fbb-a1ad-0fdb6eeb451e


Delft University of Technology

23. Chu, W. (author). Interval analysis applied to re-entry flight trajectory optimization.

Degree: Aerospace Engineering, Control and Simulation, 2007, Delft University of Technology

 <p>Trajectory optimization is an essential part of space plane mission design. One important aspect of trajectory optimization for re-entry vehicles is to minimize the total… (more)

Subjects/Keywords: interval analysis; trajectory optimization; re-entry

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APA (6th Edition):

Chu, W. (. (2007). Interval analysis applied to re-entry flight trajectory optimization. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:97730ff5-ccbf-4809-8a79-2e3856c266f4

Chicago Manual of Style (16th Edition):

Chu, W (author). “Interval analysis applied to re-entry flight trajectory optimization.” 2007. Masters Thesis, Delft University of Technology. Accessed September 22, 2020. http://resolver.tudelft.nl/uuid:97730ff5-ccbf-4809-8a79-2e3856c266f4.

MLA Handbook (7th Edition):

Chu, W (author). “Interval analysis applied to re-entry flight trajectory optimization.” 2007. Web. 22 Sep 2020.

Vancouver:

Chu W(. Interval analysis applied to re-entry flight trajectory optimization. [Internet] [Masters thesis]. Delft University of Technology; 2007. [cited 2020 Sep 22]. Available from: http://resolver.tudelft.nl/uuid:97730ff5-ccbf-4809-8a79-2e3856c266f4.

Council of Science Editors:

Chu W(. Interval analysis applied to re-entry flight trajectory optimization. [Masters Thesis]. Delft University of Technology; 2007. Available from: http://resolver.tudelft.nl/uuid:97730ff5-ccbf-4809-8a79-2e3856c266f4

.