| 质量矩复合控制拦截器一体化制导控制方法 |
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| 引用本文： | 郭庆,秦开宇,杨明.质量矩复合控制拦截器一体化制导控制方法[J].固体火箭技术,2010,33(4). |
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| 作者姓名： | 郭庆 秦开宇 杨明 |
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| 作者单位： | 1. 电子科技大学,空天科学技术研究院,临近空间联合实验室,成都,610054
2. 哈尔滨工业大学,控制与仿真中心,哈尔滨,150001 |
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| 基金项目： | 国家863创新基金项目 |
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| 摘 要： | 在建立质量矩复合控制拦截器制导控制一体化数学模型的基础上,利用微分几何策略对一体化制导控制系统进行了设计,给出了发动机期望控制力矩和滑块期望位置指令,并采用极点配置方法对反馈控制系数进行了设计。为保证系统具有能控性,对滑块质量和发动机稳态推力参数进行了设计。仿真结果表明,该方法能实现拦截器末段的制导控制,同时能降低对滑块执行机构的功率要求。
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| 关 键 词： | 质量矩复合控制拦截器 制导控制一体化 微分几何策略 极点配置 |
Integrated guidance and control method of mass moment combined control interceptor |
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| GUO Qing,QIN Kai-yu,YANG Ming.Integrated guidance and control method of mass moment combined control interceptor[J].Journal of Solid Rocket Technology,2010,33(4). |
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| Authors: | GUO Qing QIN Kai-yu YANG Ming |
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| Institution: | GUO Qing1,QIN Kai-yu1,YANG Ming2(1.Near Space Associated Lab.,University of Electronic Science and Technology of China,Chengdu 610054,2.Control and Simulation Center,Harbin Institute of Technology,Harbin 150001) |
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| Abstract: | On basis of constructing the model of integrated guidance and control,the system was designed with differential geometry game in order to supply anticipated control moments of motors and position of moving mass.Then feedback control coefficients were designed by using the method of configured apex.To realize the controllability of system,the parameters of moving object's mass and motor's steady thrust were designed.Simulation results show that this method can realize efficiently the terminal guidance of int... |
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| Keywords: | mass moment combined control interceptor integrated guidance and control method differential geometry game configured apex |
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