摘要
在旋转导弹寻的制导控制系统半实物仿真中,由于转台跟踪导弹滚动角速度??存在误差,导致半实物仿真出现显著误差,甚至失败.本文分析了这一误差对半实物仿真的影响,提出了解决办法,使半实物仿真取得了成功.
The effects of the turn table errors resulting from tracking the rolling angle velocity f of missiles on the errors occured in the Hardware-J_n-The-Loop Simulations of the Homing guidance and control systems for spanning missiles are analysed and the improving methods are also presented in this paper.
出处
《航天控制》
CSCD
北大核心
1992年第3期57-61,共5页
Aerospace Control
关键词
战术导弹
仿真
飞行模拟器
Tactical missile Simulation technique Flight Simulator
