针对一种拦截战术弹道导弹制导规律的特点,以经典的劳斯稳定判据为依据,对其制导控制回路的稳定性进行了分析。
In this study we have attempted to investigate the trajectory stability problems of head-on anti-tactical ballistic missile guidance by way of the Lawes Criterion.
数字仿真结果表明,所设计的制导控制系统耦合回路对天线罩瞄准线误差斜率的摄动具有较好的鲁棒性。
The digital simulation showed that the coupling loop in guidance control system had satisfactory robustness for the disturbance of error slope for radome's aiming line.
制导和控制一体化的设计方法充分考虑了制导和控制回路的不确定性和未建模动态。
Uncertainties and unmodelled dynamics are taking into consideration in this integrated approach to guidance and control.
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