Author:
Wu Dawei,Chen Mou,Gong Huajun
Subject
Applied Mathematics,Control and Systems Engineering,Electrical and Electronic Engineering,Computer Science Applications,Instrumentation
Reference41 articles.
1. Wilson DJ, Riley DR. Development of high angle of attack flying qualities criteria using ground-based manned simulators. In: Proceedings of the aerospace and electronics conference; 1989. NAECON 1989, Proceedings of the IEEE 1989 National, IEEE; 1989, p. 407–14.
2. Ouyang G, Ping Z, Zhao D. Control allocation design and agility evaluation for fighter post-stall pitching maneuver. In: Proceedings of the guidance, navigation and control conference; 2014, p. 1483–488.
3. High aoa flight control law design based on nonlinear dynamic inversion method;Fan;Comput Simul,2012
4. Clark M, Bernens M. High angle-of-attack flight characteristics of the yf-22. AIAA Paper; 1991. 91–3194.
5. Vladislav K, Murphy PC, Estimation of aircraft nonlinear unsteady parameters from wind tunnel data, NASA langley technical report server; 1998.
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