Parameter-dependent robust control for a rotorcraft UAV-Reference-Cited by-同舟云学术

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Parameter-dependent robust control for a rotorcraft UAV

Published:2005-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
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Author:

Voorsluijs Gerwin¹,Mulder J.A.¹

Affiliation:

1. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6407

Reference77 articles.

1. ˙-x = A-x+B-u (4) -y = C-x+D-u (5)

2. ˙-x = A-x+B-u (4) -y = C-x+D-u (5)

3. ˙-x = A-x+B-u (4) -y = C-x+D-u (5)

4. 0 0.1

5. Figure 3. Euler angles and control inputs required for equilibrium -5 0 5 10 -1 0 1β1cHR

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Trajectory planning and trajectory tracking for a small-scale helicopter in autorotation;Control Engineering Practice;2017-01

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

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