作者投稿和查稿 主编审稿 专家审稿 编委审稿 远程编辑

计算机工程 ›› 2010, Vol. 36 ›› Issue (9): 243-245. doi: 10.3969/j.issn.1000-3428.2010.09.086

• 工程应用技术与实现 • 上一篇    下一篇

基于Creator/Vega的寻的导弹飞控系统

张飞宇,闫晓勇   

  1. (北京理工大学宇航科学技术学院,北京 100081)
  • 收稿日期:1900-01-01 修回日期:1900-01-01 出版日期:2010-05-05 发布日期:2010-05-05

Homing Missile Flight Control System Based on Creator/Vega

ZHANG Fei-yu, YAN Xiao-yong   

  1. (School of Aerospace Science and Engineering, Beijing Institute of Technology, Beijing 100081)
  • Received:1900-01-01 Revised:1900-01-01 Online:2010-05-05 Published:2010-05-05

摘要:

针对寻的导弹人在回路飞控系统的设计问题,提出一种Vega/Creator视景仿真与导弹飞控系统设计相结合的设计方法。人在回路的构建采用以飞行摇杆作为指令输入、将人体动力学环节加入制导回路从而使系统闭合的方法。仿真实验结果证明,该设计不仅考察飞控系统的适应能力,而且为飞控系统的参数设计提供必要的实验依据,解决人在回路飞控系统设计的成型问题。

关键词: 视景仿真, 寻的导弹, 飞控系统, 人在回路

Abstract:

Aiming at the desigh problem of the homing missile man-in-the-loop fight control system, the method of combining Vega/Creator virtual simulation with the flight control system design is brought forward. According to the operator’s operation, the data from the stick device are real-time dealt with, the closed homing system including kinetics of human body is adopted, so the man-in-the-loop system design is formed. Simulational result shows that the adaptive capacity of flight control system can be inspected and the parameters of control system can be designed by means necessary experiments, the man-in-the-loop design problem is solved.

Key words: virtual simulation, homing missile, flight control system, man-in-the-loop

中图分类号: