Flight testing and simulation of an F-15 airplane using throttles for flight control
Author:
Affiliation:
1. NASA, Flight Research Center, Edwards, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-4109
Reference2 articles.
Cited by 5 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 Risk Management Architecture for Emergency Integrated Aircraft Control;Infotech@Aerospace 2011;2011-03-29
2. Designing for damage—robust flight control design using sliding mode techniques;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2003-05-01
3. Controlling aircraft with engine thrust only: nonlinear challenges;Nonlinear Analysis: Theory, Methods & Applications;1999-01
4. Flight testing a propulsion-controlled aircraft emergency flight control system on an F-15 airplane;Biennial Flight Test Conference;1994-06-20
5. Preliminary flight test results of a fly-by-throttle emergency flight control system on an F-15 airplane;29th Joint Propulsion Conference and Exhibit;1993-06-28
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