| 基于稳定性分析的寻的制导约束问题研究 |
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| 引用本文： | 季登高,姚郁,贺风华.基于稳定性分析的寻的制导约束问题研究[J].哈尔滨工业大学学报,2007,39(5):678-681. |
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| 作者姓名： | 季登高 姚郁 贺风华 |
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| 作者单位： | 哈尔滨丁业大学控制与仿真中心,哈尔滨,150080 |
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| 基金项目： | 国家自然科学基金资助项目(60674043) |
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| 摘 要： | 基于平面拦截模型,给出了比例导引制导系统的有限时间鲁棒绝对稳定和输入输出稳定的条件,在此基础上针对有界的任意目标机动,分析了制导系统性能对弹体动态特性、可用过载和制导规律等因素的要求,给出了制导控制系统设计的边界条件.仿真结果验证了边界条件的可行性和有效性.
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| 关 键 词： | 有限时间鲁棒绝对稳定 输入输出稳定 弹体动态 目标机动 Lurie系统 |
| 文章编号： | 0367-6234（2007）05-0678-04 |
| 修稿时间： | 2007-03-12 |
Research on design constraints of homing guidance system based on stability analysis |
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| JI Deng-gao,YAO Yu,HE Feng-hua.Research on design constraints of homing guidance system based on stability analysis[J].Journal of Harbin Institute of Technology,2007,39(5):678-681. |
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| Authors: | JI Deng-gao YAO Yu HE Feng-hua |
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| Affiliation: | Control and Simulation Center;Harbin Institute of Technology;Harbin 150080;China |
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| Abstract: | This paper studies on the finite time robust absolute stability and input-output stability of a proportional navigation guidance system based on the planar engagement geometry.Considering the random bounded target maneuver,the boundary conditions of guidance system design are obtained via the analysis of the limitations on the missile body characteristic,the available missile acceleration,the guidance law and so on.The analysis and simulation results provide the feasible theoretical basis for the design of ... |
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| Keywords: | finite time robust absolute stability input-output stability missile dynamics target maneuver Lurie system |
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