Citation: | Zhang Ping, Wang Dong, Chen Zongjiet al. PostStall Maneuver Control Law for Aircrafts with New Control Configuration[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(1): 23-26. (in Chinese) |
[1] Zwernememan W D,Eliler B G. VISTA/F-16 multi-axis thrust vectoring (MATV) law design and evaluation . AIAA-94-3513-CP,1994 [2] 廖展燕.X-31A超机动性验证机试飞[J].飞行试验,1994, 10(1):17~20 Liao Zhanyan. Flight test of the X-31A highly maneuverable testing aircraft . Flight Testing, 1994,10(1):17~20(in Chinese) [3] Durham W C. Control stick logic in high-angle-of-attack maneuvering[J]. Journal of Guidance Control and Dynamics, 1995, 18(5):170~174 [4] Gutter R, Friehmelt H, Haiplik R. Tactical utility of the X-31A using post technologies . ICAS-96-3.7.5,1996 [5] Walker L A. Flight testing the X-36-the test pilot's perspective . NASA Contract NAS 2-14269,1997 [6] 张 平,高金源. 采用扩展线性化法设计飞控系统[J]. 航空学报,1993, 14(9):A498~502 Zhang Ping, Gao Jinyuan. Flight control design using extended linearization of nonlinear systems[J]. Acta Aeronautica et Astronautica Sinica, 1993, 14(9):A498~502(in Chinese) [7] (德)布洛克毫斯·鲁道夫.飞行控制[M].北京:国防工业出版社,1999 Rudolf Brockhaus. Flight control[M]. Beijing:National Defence Industry Press, 1999(in Chinese)
|