Citation: | Kong Yinan, Wang lixin, Qian Weiqi, et al. Neural network control in active vortex control based on low aspect ratio flying wing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(06): 677-680. (in Chinese) |
[1] Praveen Joshi, John Valask. Direct comparison of neural network, fuzzy logic and model predictive variable structure vortex flow controllers . AIAA-99-4279, 1999 [2] Bernhardt J, Williams D R. Closed-loop control of forebody flow asymmetry . AIAA-95-0651, 1995 [3] 汪 清.飞机大攻角非定常气动力建模及其应用研究 .西安:西北工业大学航天工程学院,1994 Wang Qing. Unsteady aerodynamic models at high angles-of-attack and their application . Xi’an:College of Aeronautics, Northwestern Polytechnic University, 1994(in Chinese) [4] 马超,李林,王立新.大展弦比飞翼布局飞机新型操纵面设计[J].北京航空航天大学学报, 2007, 33(2):149-153 Ma Chao,Li Lin,Wang Lixin. Design of innovative control surfaces of flying wing aircrafts with large ratio aspect[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(2):149-153(in Chinese) [5] Daigoro Ito, John Valasek. Model predictive variable structure control control with model following for forebody vortex flow control . AIAA-99-4216, 1999 [6] Addington A G, Myatt J H. Control-surface deflection effects on the innovative control effectors (ICE 101) design . AFRL-VA-WP-TR-2000-30,2000
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