Translational motion control of VSTOL aircraft using nonlinear dynamic inversion-Reference-Cited by-同舟云学术

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Translational motion control of VSTOL aircraft using nonlinear dynamic inversion

Published:1995-08-07 Issue: Volume: Page:
ISSN:
Container-title:20th Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Smith P,Patel Y

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-3452

Reference9 articles.

1. Based on Dynamic Inversion', AFWAL-TR-87-3079,

2. Conference,August 1990,pp 808-825.

3. 210-222.

Cited by 4 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

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3. Robust dynamic inversion controller design and analysis for the X-38;AIAA Guidance, Navigation, and Control Conference and Exhibit;2001-08-06

4. Flight test experience of a non-linear dynamic inversion control law on the VAAC Harrier;Atmospheric Flight Mechanics Conference;2000-08-14

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