学术
摘 要:
由于大气层内动能拦截器控制系统具有非连续性、不确定性，为了提高动能拦截器控制系统的抗干扰性和机动性，设计了一种新的滑模变结构导引律。通过末制导弹道仿真，将其应用于动能拦截器末制导导引拦截三维螺旋机动目标，结果表明，滑模变结构导引律具有响应快速，简单易行，有效对付高机动目标等优点，对于KKV拦截三维螺旋机动目标有很好的鲁棒性。[著者文摘]
文章出处:
《现代防御技术》-2008年36卷1期,109 -59-61,109页
栏目信息:
分 类 号:
文献标识码:
A
文章编号:
1009-086X（2008）-01-0059-03
Research on Variable-Structure Control System with Sliding Mode Navigation Law Applied on KKV
YAN Bao-qin,JIN Yu-hua, LI Jun-long （The Second System Design Department of the Second Research Academy of CASIC, Beijing 100854, China）
Abstract:
For the discontinuity and indeterminacy of KKV control system navigation law, variable-structure control system with s the anti-disturbed ability and maneuverability of KKV liding control mode navigation, in the atmosphere, a new was designed to enhance system. Through end navigation trajectory emulator, this new navigation law was used on KKV end navigation to intercept 3D roll maneuver target The emulator results showed that variable-structure control the merits response fast, easy to realize, and powerful to system intercept with sliding mode navigation law had high maneuver target etc.. Also, ithad strong robustness for KKV to intercept 3D roll maneuver target.[著者文摘]
Key words:
variable-structure control system with sliding mode navigation law; endoatmospheric;terminal navigation; 3D roll maneuver target
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