南京理工大学学报（自然科学版）2017，Vol.41Issue(5)：562-568,7.DOI:10.14177/j.cnki.32-1397n.2017.41.05.004
一种舵面故障导弹控制分配优化方法
Control allocation optimization for missile with rudder fault
包振洲 1陈洁卿 1孙瑞胜 1祝刚2
作者信息
- 1. 南京理工大学 能源与动力工程学院,江苏 南京210094
- 2. 中国工程物理研究院 电子工程所,四川 绵阳621900
- 折叠
摘要
Abstract
The control allocation optimization of the missile with multi-control effectors under the rudder fault condition is researched and the optimization model is established. A bases-choose method based on the bases sequence control allocation is given to overcome the mutation problem due to the same effectiveness of many bases. The comparation with the traditional allocation shows that the method in this paper has the good performance of accuracy and rapidity,and it can provide the foundation of the fault-tolerant control of missiles.关键词
控制分配/基排序法/舵面故障/优化设计Key words
control allocation/bases sequence approach/rudder fault/optimization design分类
信息技术与安全科学引用本文复制引用
包振洲,陈洁卿,孙瑞胜,祝刚..一种舵面故障导弹控制分配优化方法[J].南京理工大学学报（自然科学版）,2017,41(5):562-568,7.
