Linear and Parameter-Dependent Robust Control Techniques Applied to a Helicopter UAV-Reference-Cited by-同舟云学术

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Linear and Parameter-Dependent Robust Control Techniques Applied to a Helicopter UAV

Published:2004-06-22 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
Short-container-title:

Author:

Voorsluijs Gerwin¹,Bennani Samir¹,Scherer Carsten¹

Affiliation:

1. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4909

Reference23 articles.

1. In this case, a

2. In this case, a

3. In this case, a :

4. In orderto calculate the robust performance, the system is transformedinto a representationthat allowscalculation of a µ-bound. To this extent, the performance weights are -1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.8 1

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1. Integral-based robust LPV control of nonlinear flight systems;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-07-19

2. Yaw Control of RUAVs : an Adaptive Robust H∞ Control Method;IFAC Proceedings Volumes;2008

3. Development of a Modular, Generic Helicopter Flight Dynamics Model for Real-Time Simulation;AIAA Modeling and Simulation Technologies Conference and Exhibit;2007-06-15

4. Parameter-dependent robust control for a rotorcraft UAV;AIAA Guidance, Navigation, and Control Conference and Exhibit;2005-06-19

5. Towards Vision-Based UAV Situation Awareness;AIAA Guidance, Navigation, and Control Conference and Exhibit;2005-06-19

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