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一种基于速度方向修正的旋转稳定弹弹道跟踪制导方法研究

钟扬威 王良明 张立研 叶昌 史祥鹏

弹道学报2017,Vol.29Issue(4):15-21,7.
弹道学报2017,Vol.29Issue(4):15-21,7.

一种基于速度方向修正的旋转稳定弹弹道跟踪制导方法研究

Study on Trajectory Tracking Guidance Method for Spin Stabilized Projectile Based on Velocity Direction Correction

钟扬威 1王良明 2张立研 3叶昌 1史祥鹏1

作者信息

  • 1. 中国航天科工集团 第九总体设计部,湖北 武汉430040
  • 2. 南京理工大学 能源与动力工程学院,江苏 南京210094
  • 3. 国营洛阳丹城无线电厂,河南 洛阳471000
  • 折叠

摘要

Abstract

A trajectory tracking guidance method based on velocity direction correction was proposed for the design of guidance law of spin stabilized 2D trajectory correction projectile(TCP). The laws of attack angle motion and velocity motion while the fixed canards generated step excitation were derived,and the relationships between the phase angle of average deflection angle and the roll angle of fixed canards were obtained. By generating a virtual future point on the standard trajectory, the commands of the velocity angles were obtained. The principle was proposed by correcting errors between the velocity direction and the commands,and the tracking of standard trajectory was achieved. A new standard trajectory can be generated in real time through the impact point prediction while the actual trajectory is far away from the standard trajectory. The simulation results show that,when the firing angle is small,the velocity direction correction can be used to track the standard trajectory on the whole trajectory. When the firing angle is large, the standard trajectory can be generated on downward phase, and then the velocity direction correction can be used to track the new standard trajectory.

关键词

旋转稳定弹/角运动/弹道/制导

Key words

spin stabilized projectile/angular motion/trajectory/guidance

分类

军事科技

引用本文复制引用

钟扬威,王良明,张立研,叶昌,史祥鹏..一种基于速度方向修正的旋转稳定弹弹道跟踪制导方法研究[J].弹道学报,2017,29(4):15-21,7.

基金项目

十三五装备预研基金项目(0715A) (0715A)

弹道学报

OA北大核心CSCDCSTPCD

1004-499X

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