再入方式
In this paper, basing on three-axis's stable dynamic equations of moving centroid reentry vehicles, the dynamic inversion controller was designed under three-axis's stable control mode.
在推导三通道稳定再入飞行器动力学方程的基础上,运用动态逆控制理论设计了三通道稳定模式下变质心再入飞行器的控制系统。
The Unified Guidance Mode of the Disturbing Multiple Independently Targetable Reentry Vehicles and Single Head
摄动多头分导与单弹头制导的统一模式
Reentry Mode Simulation and Analysis of Manned Deep Space Exploration
载人深空飞行返回再入模式仿真研究
Results of demonstration shown: for the fundamental guidance equation can be used the unified mode of the disturbing guidance in relation to the single head, rocket vehicles and the multiple independently targetable reentry vehicles, not be necessary for develop various modes.
论证结果表明:对基本制导方程来说,单弹头、运载火箭以及多弹头分导的摄动制导可以在同一个模型之下统一起来,而不必各自拟定不同的方案。
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