Trajectory Correction Strategy based on Relative Deviation between Projectile and Target

被引:0
|
作者
Liu, Jingtao [1 ]
Li, Dongguang [1 ]
Zhang, Cong [1 ]
机构
[1] Beijing Inst Technol, Sch Mechatron Engn, Beijing, Peoples R China
关键词
trajectory correction; fligh echanics; correction Nfraiegy; SPINNING MISSILES; STABILITY;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
For a higher accuracy of projectiles, trajectory correction fuze is proposed. In this design, sensors and actuators are pre-designed and optimized. Based on the projectile flight model, the working principle of trajectory correction is explained, and the trajectory correction strategy is proposed. In the trajectory correction strategy, the detection deviation and the response of the correction actuator arc analyzed. The effect of the strategy is verified by the example of closed-loop simulation. The results show that the accuracy of this method is obviously improved, which is suitable for the terminal correction of mortars.
引用
收藏
页码:581 / 586
页数:6
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