| 导弹质量矩控制技术建模与静态性能分析 |
| |
| 引用本文： | 周韬,黄运平,陈万春,殷兴良.导弹质量矩控制技术建模与静态性能分析[J].宇航学报,2006,27(5):1081-1086. |
| |
| 作者姓名： | 周韬 黄运平 陈万春 殷兴良 |
| |
| 作者单位： | 1. 北京航空航天大学宇航学院,北京,100083
2. 中国航天科工集团公司,北京,100830 |
| |
| 摘 要： | 导弹为获得高超声速和高机动能力，必然在操纵、控制方面付出一定代价。针对所面临的困难，提出了质量矩控制方案。在分析了本方案优点的基础上，建立了质量矩控制导弹的动力学模型，包括质心动力学和绕质心的动力学方程。最后对质量矩控制模型进行数字仿真，对给出的滑块运动规律得出了三通道控制的多种响应曲线。尽管相对实际情况进行了一定简化，但是从静态控制模型获得的性能指标，已经能够证实本方案的可行性。
|
| 关 键 词： | 质量矩控制导弹 动力学建模 高超声速飞行器 |
| 文章编号： | 1000-1328（2006）05-1081-06 |
| 收稿时间： | 05 15 2006 12:00AM |
| 修稿时间： | 2006-05-152006-07-20 |
Dynamics Modeling and Static Capability Analyze of Moving Mass Trim Control of Missile |
| |
| ZHOU Tao,HUANG Yun-ping,CHEN Wan-chun,YIN Xing-liang.Dynamics Modeling and Static Capability Analyze of Moving Mass Trim Control of Missile[J].Journal of Astronautics,2006,27(5):1081-1086. |
| |
| Authors: | ZHOU Tao HUANG Yun-ping CHEN Wan-chun YIN Xing-liang |
| |
| Institution: | 1. School of Astronautics, Beihang University, Beijing 100083, China; 2. China Aerospace Science and Industry Corporation, Beijing 100830, China |
| |
| Abstract: | A research of the techniques for controlling missiles with high supersonic speed and high maneuverability was carried out in this paper,and we put forward a scheme of moving mass trim controller(MMTC) of missiles.On basis of analyzing the advantages of the scheme,a dynamics model of MMTC was constructed,which includes centroid dynamics and dynamics moment equations of centroid.Finally,digitally simulated model of MMTC,obtained some responding curves of control system for the assigned moving mass.Although the simulation was simplified compared with actual situation,the static capability index obtained from the simulation had proved the feasibility of this control scheme. |
| |
| Keywords: | Moving mass trim control missile Dynamics modeling Hypersonic vehiclc |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
