| 反舰导弹变系数修正比例导引研究 |
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| 引用本文： | 王凤莲,顾文锦.反舰导弹变系数修正比例导引研究[J].飞行力学,2003,21(1):51-54. |
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| 作者姓名： | 王凤莲 顾文锦 |
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| 作者单位： | 海军航空工程学院自动控制系, 山东烟台,264001 |
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| 摘 要： | 针对超音速反舰导弹自导段控制的特点，对比分析了两种典型的非线性导引规律即反馈线性化（FLGL）导引律和逆向接近导引律的优缺点，提出了一种称为变系数修正比例导引的方法，通过对其全弹道仿真结果的分析，说明所提出的导引规律是正确的，具有良好的应用效果。
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| 关 键 词： | 超音速反舰导弹 过载控制 非线性导引律 比例导引 变系数修正 |
| 文章编号： | 1002-0853(2003)01-0051-04 |
| 修稿时间： | 2002年4月5日 |
Research on Amendatory Proportional Navigation with Variable Coefficient of Anti-Ship Missile |
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| WANG Feng lian,GU Wen jin.Research on Amendatory Proportional Navigation with Variable Coefficient of Anti-Ship Missile[J].Flight Dynamics,2003,21(1):51-54. |
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| Authors: | WANG Feng lian GU Wen jin |
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| Abstract: | Based on the characteristics of the self guidance phase for the supersonic anti ship missile, their advantages and disadvangtages between two typical nonlinear guidance laws, such as 'Feedback Linear Guidance Law' and 'Nonlinear Inverse Approach', are introduced in this paper. Then the amendatory proportional navigation with variable coefficient has been given. The analysis of the simulation results of the whole trajectory of the missile shows that this law is mostly effective. |
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| Keywords: | supersonic anti ship missile overload control nonlinear guidance law proportional navigation amendatory proportional navigation with variable coefficient |
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