Electronics Optics & Control, Volume. 23, Issue 11, 27(2016)
Dynamic Matrix Control for Fighter Envelope Protection
[2] [2] U.S.Department of Transportation Federal Aviation Administration.Simulation and flight test assessment of safety benefits and certification aspects of advanced flight control systems[R].Springfield: U.S.Public Through the National Technical Information Service(NTIS), 2003.
[3] [3] HORN J F, CALISE A J, PRASAD J V R.Flight envelope limit detection and avoidance for rotorcraft[J].Journal of the American Helicopter Society, 2002, 47(4): 253-262.
[5] [5] PRASAD J V R, YAVRUCUK I, UNNIKRISHNAN S.Adaptive limit prediction and avoidance for rotorcraft[C]//Proceedings of the 28th European Rotorcraft Forum, Royal Aeronautical Society, London, 2002: 881-887.
[6] [6] STEINBERG M L.A comparison of intelligent, adaptive, and nonlinear flight control laws[C]//AIAA Gui-dance, Navi-gation, and Control Conference and Exhibit, Portland, 1999: 9-11.
[7] [7] MALINOWSKI A, ZURADA J M, LILLY J H.Inverse control of nonlinear system using neural network observer and inverse mapping approach [C]//IEEE International Conference on Neural Networks, 1995: 2513-2518.
Get Citation
Copy Citation Text
ZHENG Xin-rui, WU Qing-xian, YE Hui. Dynamic Matrix Control for Fighter Envelope Protection[J]. Electronics Optics & Control, 2016, 23(11): 27
Category:
Received: Oct. 9, 2015
Accepted: --
Published Online: Nov. 30, 2016
The Author Email: