Time-Delay Control for Integrated Missile Guidance and Control

机译：导弹制导与控制的时滞控制

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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.

机译：在本文中，开发了使用时滞控制的综合导弹制导和控制系统。下一代导弹需要拦截器以小的失误距离击中目标机动，并且重量更轻以降低成本。如果集成控制器可以利用制导子系统和控制子系统之间存在的协同作用，则有可能。时滞控制律是非线性系统的鲁棒控制技术，其结构非常简单。延时控制的特征是使用一步延时来直接估计未知动态和意外干扰。为了研究集成控制器的性能，将数值模拟作为目标的运动进行。结果表明，该综合制导控制系统具有一定的性能。

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来源
《Third Asia-Pacific International Symposium on Aerospace Technology》|2011年|1-9|共9页
会议地点 Melbourne(AU)
作者
Bong-Gyun Park; Tae-Hun Kim; Min-Jea Tahk;
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作者单位

Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), Daejon, Republic of Korea;

Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), Daejon, Republic of Korea;

Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), Daejon, Republic of Korea;

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会议组织
原文格式 PDF
正文语种 eng
中图分类航空;航天（宇宙航行）;
关键词
Time-Delay Control; Autopilot; Guidance Law; Integrated Guidance and Control.;

机译：延时控制;自动驾驶;指导律;综合制导与控制;

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Time-Delay Control for Integrated Missile Guidance and Control

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