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| 导弹非线性控制系统的自适应规律 | |
| 引用本文： | 姚勤,陆建军,李伟忠,赵峰.导弹非线性控制系统的自适应规律[J].上海航天,2005,22(5):34-37. |
| 作者姓名： | 姚勤 陆建军 李伟忠 赵峰 |
| 作者单位： | 1. 国防科学技术大学,航天与材料工程学院,湖南,长沙,410073 2. 中国人民解放军驻上海精密仪器研究所军代室,上海,200233 3. 中国人民解放军海军驻上海地区航天系统军事代表室,上海,200235 |
| 摘 要： | 为简化非线性控制系统．研究了某导弹控制系统的自适应规律。给出了系统的自振方程和负倒幅特性函数．推导了非线性系统的等效线性过程，分析了系统等效增益与自振振幅的关系。获得了系统的自适应及自补偿规律。 |
| 关 键 词： | 非线性控制系统 自适应 自振方程 负倒幅特性 等效增益 自振振幅 |
| 文章编号： | 1006-1630（2005）05-0034-04 |
| 收稿时间： | 2005-05-17 |
| 修稿时间： | 2005-06-20 |
The Analysis on Self-Adaptation Rule in Non-Linear Control System for Missile |
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| YAO Qin,LU Jian-jun,LI Wei-zhong,ZHAO Feng.The Analysis on Self-Adaptation Rule in Non-Linear Control System for Missile[J].Aerospace Shanghai,2005,22(5):34-37. | |
| Authors: | YAO Qin LU Jian-jun LI Wei-zhong ZHAO Feng |
| Institution: | 1. College of Aerospace and Material Engineering, NUDT, Changsha Hunan 410073, China; 2. CPLA Rep. Office in Shanghai Institute of Precision Instruments, Shanghai 200233, China; 3. CPLA Rep. Navy Office in Shanghai Aerospace System, Shanghai 200235, China |
| Abstract: | The self-adaptation rule was studied to simplify the non-linear control system for some missile in this paper. The self-oscillation equation and negative reciprocal of AF properties function for the system were given. The equivalent linearity of non-linear system was also derived. The relationship of equivalent gain and self-oscillation amplitude was analyzed. At last, the rules of self-adaptation and self-compensation for the system were obtained. |
| Keywords: | Non-linear control system Self-adaptation Self-oscillation equation Negative reciprocal of AF properties Equivalent gain Self-oscillation amplitude |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |