[1]陈伟[],冯高鹏[],孙传杰[],等. 针对移动目标的简控弹制导控制方法研究[J].计算机技术与发展,2016,26(11):121-124.
　CHEN Wei[],FENG Gao-peng[],SUN Chuan-jie[],et al. Research on Guidance and Control Method of Simple Control Rocket-projectile for Moving Target[J].,2016,26(11):121-124.
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 针对移动目标的简控弹制导控制方法研究()
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《计算机技术与发展》[ISSN:1006-6977/CN:61-1281/TN]

卷:
26
期数:
2016年11期
页码:
121-124
栏目:
应用开发研究
出版日期:
2016-11-10

文章信息/Info

Title:
 Research on Guidance and Control Method of Simple Control Rocket-projectile for Moving Target
文章编号:
1673-629X（2016)11-0121-04
作者:
 陈伟[1]; 冯高鹏[1]; 孙传杰[1]; 薛晓中[2]
1. 中国工程物理研究院 总体工程研究所；2.南京理工大学 能源与动力工程学院
Author(s):
 CHEN Wei[1]; FENG Gao-peng[1]; SUN Chuan-jie[1]; XUE Xiao-zhong[2]
关键词:
 ; 火箭弹; 简易制导; 比例导引; STT
Keywords:
 ; rocket projectile; simple guidance; proportional guidance; STT
分类号:
TP273
文献标志码:
A
摘要:
 为降低单兵制导火箭弹的成本，同时确保其具有较远的作用距离和较高的命中精度，针对移动目标，进行单兵火箭弹简易制导控制律设计。将飞行弹道进行分段设计，分为筒内运动段、惯性飞行段和导引飞行段。在发射前通过弹载系统和测距仪对目标移动速度进行估计，采用比例导引法实现对目标的跟踪。接下来对STT控制器进行设计，基于典型设计点处控制器参数插值得到不同飞行速度下的控制器参数，确保火箭弹在整个飞行过程中具有较高的控制精度。通过仿真分析可知，所设计的制导控制系统具有较高的鲁棒性。
Abstract:
To reduce the cost of guided individual rocket projectile and ensure that it has a longer striking distance and higher accuracy at the same time,the simple guidance control law of the individual rocket projectile is designed for moving target. The flight trajectory is segmented,including barrel movement segment,inertial flight segment and guiding flight segment. Before launching the speed of the tar-get is estimated by the onboard system and rangefinder,to achieve the goal of tracking by the proportional guidance method. Then the STT controller is designed to ensure the rocket has higher control accuracy based on the controller gains of the typical design points,and the controller gains under different speed are obtained using the interpolation method. Through he simulation analysis,the result shows that the designed guidance control system has high robustness.

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更新日期/Last Update: 2016-12-13