TANG Shan-tong,LI Zhong-ying.A guidance law of variable structure adaptive for missile following its optimal nominal trajectory[J].Systems Engineering and Electronics,2002,24(7):68-76.(in Chinese)
[3]
BOUADI H,CAMINO F M.Aircraft trajectory tracking by nonlinear spatial inversion,AIAA 2012-4613[R].2012.
[4]
PU Z Q,TAN X M,FAN G L,et al.Design of entry trajectory tracking law for a hypersonic vehicle via inversion control[C]//Proc of the 10th World Congress on Intelligent Control and Automation.Beijing:IEEE,2012:1 092-1 097.
[5]
DROUOT A,RICHARD E,BOUTAYEB M.Nonlinear backstepping based trajectory tracking control of a gun launched micro aerial vehicle,AIAA 2012-4455[R].2012.
WANG Jun-bo,QU Xin,REN Zhang.Hybrid reentry guidance based on the online trajectory planning[J].Journal of Astronautics,2012,33(9):1 217-1 224.(in Chinese)
[8]
PARK S,DEYST J,HOW J P.A new nonlinear guidance logic for trajectory tracking,AIAA 2004-4900[R].2004.
[9]
DUKEMAN G A.Profile-following entry guidance using linear quadratic regulator theory,AIAA 2002-4457[R].2002.
[10]
ZHOU W Y,TAN S J,CHEN H B.A simple reentry trajectory generation and tracking scheme for common aero vehicle,AIAA 2012-4709[R].2012.
[11]
LEVY M,SHIMA T,GUTMAN S.Linear quadratic integrated versus separated autopilot-guidance design[J].Journal of Guidance,Control,and Dynamics,2013,36(6):1 722-1 730.
YANG Xi-xiang,ZHANG Wei-hua.Midcourse guidance law optimal design for air-to-air missiles based on Gauss pseudospectral method[J].Journal of National University of Defense Technology,2013,35(1):28-32.(in Chinese)
LIU Heng-jun,JIANG Huan,CHEN Wan-chun.Application of MDO algorithm to multi-tier trajectory optimization design for a surface-to-air missile kinetic kill[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(2):145-149.(in Chinese)
[18]
李殿璞.非线性控制系统[M].西安:西北工业大学出版社,2009.
[19]
LI Dian-pu.Nonlinear control system[M].Xi’an:Northwestern Polytechnical University Press,2009.(in Chinese)
[20]
李新国,方群.有翼导弹飞行动力学[M].西安:西北工业大学出版社,2005.
[21]
LI Xin-guo,FANG Qun.Flight dynamics of winged missile[M].Xi’an:Northwestern Polytechnical University Press,2005.(in Chinese)
