摘要
对寻的制导系统半实物仿真时转台如何模拟真实的弹体角运动问题进行了研究。指出了仿真实验室目标阵面视角范围的限制以及三轴转台模拟弹体角运动存在的问题对仿真的影响，并通过引入动参考坐标系以及相应的坐标转换提出了解决问题的方法，对实现方法的不足也作了相应的说明。实践证明，该方法是简单可行的。
In this document the author gives a study on the simulation of missile angular motion by simulator during the semi objective simulation of homing guidance system. Influence upon simulation is pointed out because of the limitation of visual angle on the square formation of the target in laboratory and the problem of simulation of missile angular motion by thrce axis revol ving table. The solving method is raised through presenting dynamic coordinate system and relevant changes of coordinate system. Shortcoming of the realising method is also explained in this document. The method is proved to be easy and feasible from practice.
出处
《上海航天》
1997年第6期29-32,共4页
Aerospace Shanghai
关键词
仿真
坐标系
寻的制导导弹
半实物仿真
Simulation Coordinate system Missile homing guidance Semi objective simulation
