X-29A flight control system design experiences
Author:
Affiliation:
1. Grumman Aerospace Corp., Bethpage, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-1538
Reference11 articles.
1. Application of Lagrange Optimization to the drag polar utilizing experimental data
2. Rothschild, D.and Krindler,E."Implicit Model Decoupling Approach to VTOL Flight Control Design,ITGrumman Aerospace, Bethpage, N .Y., Grumman Research Department Report RE-469, January 1974.
3. Morse, A. S. "Structure and Design of Linear Model Following Systems,111EEE Transactions on Automatic Control, Vol.AC-18, August 1973, pp.346-354.
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
1. A case for pseudo-steady aerodynamic behaviour at high motion rates;35th Aerospace Sciences Meeting and Exhibit;1997-01-06
2. Optimization-based linear and nonlinear design methodologies for aircraft control. II - Final simulations;Astrodynamics Conference;1992-08-10
3. Integrated thrust vectoring on the X-29A;Aircraft Design, Systems and Operations Conference;1988-08-17
4. X-29A flight control system performance during flight test;Aircraft Design, Systems and Operations Meeting;1987-08-17
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