Practical Methods for Aircraft and Rotorcraft Flight Control Design: An Optimization-Based Approach-Reference-Cited by-同舟云学术

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Practical Methods for Aircraft and Rotorcraft Flight Control Design: An Optimization-Based Approach

Published:2017-01-20 Issue: Volume: Page:
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Author:

Tischler Mark B.,Berger Tom,Ivler Christina M.,Mansur Mohammadreza H.,Cheung Kenny K.,Soong Jonathan Y.

Publisher

American Institute of Aeronautics and Astronautics, Inc.

Cited by 46 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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2. Commonalities between robust hybrid incremental nonlinear dynamic inversion and proportional-integral-derivative flight control law design;Aerospace Science and Technology;2024-09

3. Total Energy-Based Control Design and Optimization for Lift-Plus-Cruise Aircraft;Journal of Guidance, Control, and Dynamics;2024-07

4. Full-Envelope Flight Control for Compound Vertical Takeoff and Landing Aircraft;Journal of Guidance, Control, and Dynamics;2024-04-25

5. Design, Control Law Development, and Flight Testing of a Subscale Lift-Plus-Cruise Aircraft;AIAA SCITECH 2024 Forum;2024-01-04

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