基于滑模控制的导弹制导控制一体化设计  

Integrated Design of Missile Guidance and Control Based on Sliding-mode Control

作　　者：苗昊春[1,2] 马清华 陈韵 程冬 

机构地区：[1]清华大学自动化系,北京100084 [2]中国兵器工业第203研究所,西安710065

出　　处：《弹箭与制导学报》2011年第3期6-10,共5页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：文中对某滚转稳定反坦克导弹的俯仰和偏航通道建立了制导控制一体化数学模型,在末制导段分别采用经典方法和一体化方法设计了滑模制导律(SMG)和自适应滑模一体化制导控制律(SMGC),建立了基于dSPACE的半实物仿真系统,并对两种制导律进行了数字和半实物仿真,结果表明:一体化方法优于传统方法,可有效提高导弹制导性能。Integrated guidance and control models in pitch and yaw channels were built on a roll stable anti tank missile in tiffs pa per. Conventional and . integrated methods were used respectively to design the sliding-mode guidance （SMG） law and the integrat ed guidance and control of adaptive sliding-mode（SMGC） in the terminal guidance session. The hardware-in-the-loop based on dSPACE was established and the SMG and SMGC laws were simulated. The results indicate that the integrated method is better than the conventional and the guidance performance has been proved effectively.

关 键 词：滑模控制 制导控制一体化 DSPACE 半实物仿真 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]