海军航空工程学院学报2011，Vol.26Issue(4)：410-413,4.
基于攻角可测的不确定导弹系统的滑模自适应控制研究
Research on the Uncertain Missile System Based on Adaptive Sliding Mode Control
任晓军 1李翊 2孙晓燕 3薛建海4
作者信息
- 1. 海军驻航天科工集团三院军事代表室,北京100074
- 2. 海军装备部,西安710054
- 3. 海军航空工程学院基础部,山东烟台264001
- 4. 91049部队,山东青岛266000
- 折叠
摘要
Abstract
Considering the uncertainties caused by pneumatic parameters and model linearization of missile a kind of adaptive sliding mode control method was designed based on the combination of adaptive method and VSC method. Especially, the coefficient of the missile actuator was unknown because of the uncertain aero-coefficients, so a single adaptive item was adopted to compensate the unknown coefficient of actuator Finally, by constructing a Lyapunov function the stability of the system was proved. Some simulations were done to give examples, which showed the effectiveness of the proposed method关键词
导弹控制/滑模/自适应/不确定性Key words
missile control/sliding mode/adaptive/uncertainty分类
军事科技引用本文复制引用
任晓军,李翊,孙晓燕,薛建海..基于攻角可测的不确定导弹系统的滑模自适应控制研究[J].海军航空工程学院学报,2011,26(4):410-413,4.
