Command Optimization for Missile Roll Autopilot

摘要：

　　As command optimization for missile roll autopilot has long been neglected by missile control engineers,this paper introduces two roll command optimization methods for missile 180° rotation.First,problems in roll autopilot design are stated and the importance of command optimization is illustrated.Second,linear and exponent command optimization methods are established with the quickly and efficient method of optimization time constant provided at the same time.Then compared with each other,the advantages and disadvantages are listed for the two optimization methods.At last,the conclusion about how to choose optimization method is deduced.

关键词： Linear Optimization Exponent Optimization Roll autopilot

作者: Cui Xiaoxi Lou Yingming Wu Tao Zhang Dongxiang Wang Linping Zhang Nan

作者单位: North China Institute of Navigation and Control, Beijing 100089 Ordnance Science and Research Academy of China, Beijing 100089

会议类型: 国际会议

会议名称: the 25th Chinese Control and Decision Conference(第25届中国控制与决策会议)

会议地点: 贵阳

会议语种:英文

页码: 3509-3512

在线出版日期: 2013-05-01（万方平台首次上网日期，不代表论文的发表时间）