JIANG Xiu-qiang.One for the attacking of unmanned aerial vehicles at the end of the missile guidance law[J].Journal of Tactical Missile Technology,2013(1):87-92.(in Chinese)
[10]
王善敏,姜长生.空空导弹三维智能滑模导引律设计[J].航空兵器,2009(6):8-12.
[11]
WANG Shan-min,JIANG Chang-sheng.3D air-to-air missile intelligent sliding-mode guidance law design[J].Aviation Weapon,2009(6):8-12.(in Chinese)
[12]
王志清,李小兵,卓启明.智能滑模变结构制导律[J].上海航天,2011(1):32-36.
[13]
WANG Zhi-qing,LI Xiao-bing,ZHUO Qi-ming.Intelligent sliding mode variable structure guidance law[J].Journal of Shanghai Aerospace,2011(1):32-36.(in Chinese)
CHEN Peng,ZHU Zhan-xia.Sliding mode method in the application of air-to-air missile guidance law[J].Journal of Flight Mechanics,2013,4(2):135-138.(in Chinese)