Time-Delay Control for Integrated Missile Guidance and Control

摘要：

In this paper, integrated missile guidance and control systems using time-delay control are developed. The next generation missile requires that an interceptor hits the target maneuvering with small miss distances and has lower weight to reduce costs. That is possible that if the synergism existing between the guidance and control subsystems is exploited by the integrated controller. The time-delay control law is a robust control technique for nonlinear systems and has a very simple structure. The feature of time-delay control is to directly estimate the unknown dynamics and the unexpected disturbance using one step time delay. To investigate the performance of the integrated controller, numerical simulations are performed as the motion of the target. The results show that the integrated guidance and control system has a performance.

关键词： Time-Delay Control Autopilot Guidance Law Integrated Guidance and Control.

作者: Bong-Gyun Park Tae-Hun Kim Min-Jea Tahk

作者单位: Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), Daejon, Republic of Korea

会议类型: 国际会议

会议名称: 2011年亚太航空航天技术学术会议(APISAT 2011)

会议地点: 澳大利亚

会议语种:英文

页码: 1-9

在线出版日期: 2011-02-28（万方平台首次上网日期，不代表论文的发表时间）