一种舵面故障导弹控制分配优化方法  

Control allocation optimization for missile with rudder fault

作　　者：包振洲 陈洁卿[1] 孙瑞胜[1] 祝刚[2] 

机构地区：[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

出　　处：《南京理工大学学报》2017年第5期562-568,共7页Journal of Nanjing University of Science and Technology

摘　　要：该文研究了一种多操纵面导弹舵面故障情况下的控制分配优化设计方法,建立了相应的控制分配优化模型。针对由于多组基底效率相同产生的控制分配结果的跳变问题,基于基排序思想提出了一种基底选择方法。通过与传统分配方法的分配结果进行比较,验证了该文方法的有效性和灵活性。该文结果可为导弹的容错控制提供基础。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 problemdue 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 

分 类 号：TP273[自动化与计算机技术—检测技术与自动化装置]