Li Z F. Special wind tunnel testing technology[M]. Beijing: Aviation Industry Press, 2010: 562-563.(in Chinese) 李周复. 风洞特种试验技术[M]. 北京: 航空工业出版社, 2010: 562-563.
[2]
Gao G H. Research on multi-path planning problem in large area[D]. Changsha: College of Mechatronic Engineering and Automation, National University of Defense Technology, 1999.(in Chinese) 高国华. 大范围多路径规划问题研究[D]. 长沙: 国防科学技术大学机电工程与自动化学院, 1999.
[3]
Betts J T. Survey of numerical methods for trajectory optimization[J]. Journal of Guidance, Control, and Dynamics, 1998, 21(2): 193-207.
[4]
Murayama M, Togashi F, Nakahashi K. Simulation of aircraft response to control surface deflection using unstructured dynamic grids, AIAA-2002-2940[R]. Reston: AIAA, 2002.
[5]
Yong E M, Chen L, Tang G J. Survey of aircraft trajectory optimization methods[J]. Journal of Astronautics, 2008, 29(2): 398-406. (in Chinese) 雍恩米, 陈磊, 唐国金. 飞行器轨迹优化数值方法综述[J]. 宇航学报, 2008, 29(2): 398-406.
[6]
Huang G Q, Lu Y P, Nan Y. A survey of numerical algorithms for trajectory optimization of flight vehicles[J]. Sci China Tech Sci, 2012, 42(9): 1016-1036. (in Chinese) 黄国强, 陆宇平, 南英. 飞行器轨迹优化数值算法综述[J]. 中国科学: 技术科学, 2012, 42(9): 1016-1036.
[7]
Yang K, Sukkarieh S, Kang Y. Adaptive nonlinear model predictive path tracking control for a fixed-wing unmanned aerial vehicle, AIAA-2009-5622[R]. Reston: AIAA, 2009.
[8]
Schütte A, Einarsson G, Raichle A, et al. Prediction of the unsteady behavior of maneuvering aircraft by CFD aerodynamic,flight-mechanic and aeroelastic coupling, NATO RTO-MP-AVT-123-P-11[R]. Neuilly sur Seine, France: NATO Research and Technology Organization, 2005.
[9]
Zhang Y, Chen J, Shen L C. Real-time trajectory planning for UCAV air-to-surface attack using inverse dynamics optimization method and receding horizon control[J]. Chinese Journal of Aeronautics, 2013, 26(4): 1038-1056.
[10]
Huntington G T. Advancement and analysis of Gauss pseudospectral transcription for optimal control problems[D]. Cambridge: Department of Aeronautics and Astronautics, Massachusettes Institute of Technology, 2007.
[11]
Zhang Y, Chen J, Shen L C. Hybrid hierarchical trajectory planning for a fixed-wing UCAV performing air-to-surface multi-target attack[J]. Journal of Systems Engineering and Electronics, 2012, 23(4): 536-552.
[12]
Zhang Y, Zhang W P, Chen J, et al. Air-to-ground weapon delivery trajectory planning for UCAVs using Gauss pseudospectral method[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(7): 1240-1251. (in Chinese) 张煜, 张万鹏, 陈璟, 等. 基于Gauss伪谱法的UCAV对地攻击武器投放轨迹规划[J]. 航空学报, 2011, 32(7): 1240-1251.
[13]
Yong E M, Tang G J, Chen L. Rapid trajectory optimization [JP2]for hypersonic reentry vehicle via Gauss pseudospectral[JP] method[J]. Journal of Astronautics, 2008, 29(6): 1766-1772. (in Chinese) 雍恩米, 唐国金, 陈磊. 基于Gauss伪谱方法的高超声速飞行器再入轨迹快速优化[J]. 宇航学报, 2008, 29(6): 1766-1772.
[14]
Liu H F, Chen S F, Shen L C, et al. Tactical trajectory planning for stealth unmanned aerial vehicle to win the radar game[J]. Defence Science Journal, 2012, 62(6): 375-381.
[15]
Chen S F, Liu H F, Shen L C, et al. Penetration trajectory planning based on radar tracking features for UAV[J]. Aircraft Engineering and Aerospace Technology, 2012, 85(1): 62-71.
[16]
Milam M B. Real-time optimal trajectory generation for constrained dynamical systems[D]. Pasadena: California Institute of Technology, 2003.
[17]
Boelens O J, Prananta B B, Soemrwoto B I. Towards an aero-servo-elastic simulation capability for high-performance fighter aircraft, NATO RTO-MP-AVT-123-P-30[R]. Neuilly sur Seine, France: NATO Research and Technology Organization, 2005.
[18]
Schütte A, Einarsson G. Numerical simulation of maneuvering aircraft by aerodynamic flight-mechanic and structural mechanics coupling[J]. Journal of Aircraft, 2009, 46(1): 53-64.
[19]
McDaniel D R, Sears D R, Tuckey T R, et al. Aerodynamic control surface implementation in Kestrel v2.0, AIAA-2011-1175[R]. Reston: AIAA, 2011.
[20]
Morton S A, Eymann T A, Lamberson S, et al. Relative motion simulations using an overset multimesh paradigm with Kestrel v3, AIAA-2012-0712[R]. Reston: AIAA, 2012.
[21]
Green B E. Analysis of the stability and control characteristics of the F/A-18E super hornet using the Kestrel CFD flower solver, AIAA-2012-0715[R]. Reston: AIAA, 2012.
[22]
Cummings R M, Schütte A. An integrated computational/experimental approach to UCAV stability and control estimation: overview of NATO RTO AVT-161, AIAA-2010-4392[R]. Reston: AIAA, 2010.
[23]
Frazzoli E. Robust hybrid control for autonomous vehicle motion planning[D]. Cambridge: Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 2001.
[24]
Air force mission support system (AFMSS)[EB/OL]. (1999-01-09)[2012-11-07].
[25]
AN-SYQ-21 Tactical automated mission planning system (TAMPS)[EB/OL]. (1999-01-11) [2012-11-07].
[26]
htm.
[27]
AN/TYQ-77 Aviation mission planning system (AMPS)[EB/OL]. (2011-07-07) [2012-11-07].
Tao Y, Fan Z L, Wu J F. CFD based virtual flight simulation of square cross-section missile with control in longitudinal flight[J]. Chinese Journal of Theoretical and Applied Mechanics, 2010, 42(2): 169-176. (in Chinese) 陶洋, 范召林, 吴继飞. 基于CFD的方形截面导弹纵向虚拟飞行模拟[J]. 力学学报, 2010, 42(2): 169-176.
[31]
Da X Y, Tao Y, Zhao Z L. Numerical simulation of virtual flight based on prediction-correction coupling method and chimera grid[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(6): 977-983.(in Chinese) 达兴亚, 陶洋, 赵忠良. 基于预估校正和嵌套网格的虚拟飞行数值模拟[J]. 航空学报, 2012, 33(6): 977-983.
[32]
Leavitt C A. Real-time in-flight planning[C]//Proceedings of the IEEE 1996 National Aerospace and Electronics Conferenc, 1996, 1: 83-89.
Zhang Y. Research on air-to-ground attack trajectory planning for combat aircraft[D]. Changsha: College of Mechatronic Engineering and Automation, National University of Defense Technology, 2012. (in Chinese) 张煜. 作战飞机空对地攻击轨迹规划技术研究[D]. 长沙: 国防科学技术大学机电工程与自动化学院, 2012.
[35]
HELIPSYS[EB/OL]. [2013-12-09].
[36]
Li X L, Yang Y. Numerical simulation of the free rolling motion of a delta wing configuration with aileron deflection[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(3): 453-462.(in Chinese) 李喜乐, 杨永. 带副翼偏转的三角翼自由滚转运动数值模拟[J]. 航空学报, 2012, 33(3): 453-462.