A Novel Analysis for Tactical Missile Autopilot Topologies

摘要：

The available feedback topologies for tactical missile autopilot were detailed and examined using optimal control. There were transformations that could provide equivalent closed loop properties for the different topologies. The open loop properties of autopilots would be different, however. Compared with the limitations of traditional stability margins, a novel vector margin approach was introduced to establish a standard performance level and determine the best autopilot topology from a robustness perspective. A static unstable plant as example was used throughout. The analysis and simulation results validate the presented approach.

关键词： Missile Autopilot Robustness Vector Margin Optimal Control

作者: FAN Jun-fang SUN Bao-cai SU Zhong DONG Si-yu

作者单位: Institute of Intelligence Control, Beijing Information Science & Technology University, Beijing, Chi Research Institute on General Development and Evaluation of Equipment, AFEA, Beijing, China School o Department of Computer Engineering, Ordnance Engineering College of PLA; Shijiazhuang, China

会议类型: 国际会议

会议名称: The 31st Chinese Control Conference(第三十一届中国控制会议)

会议地点: 合肥

会议语种:英文

页码: 2316-2320

在线出版日期: 2012-07-01（万方平台首次上网日期，不代表论文的发表时间）