three-dimensional reentry trajectory 三维再入轨迹
optimal reentry trajectory 最优再入轨道
standard reentry trajectory 标准再入轨道
reentry trajectory optimization 再入弹道优化
Maneuverable Reentry Trajectory 再入机动弹道
reference trajectory reentry guidance [航] 基准轨道再入制导
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Spacecraft reentry trajectory optimization is a kind of optimal control problem.
飞行器再入轨迹优化是一类最优控制问题。
The designed maneuver reentry trajectory can meet the demands of attitude, heat flux and velocity for the warhead.
所设计的再入机动弹道能满足机动弹头对姿态、热流和速度的要求。
In view of the particularity for maneuver warhead reentry trajectory and the guidance method, key techniques in attitude control system design are analyzed.
针对机动弹头再入弹道和制导方式的特殊性，分析了激光末制导机动弹头姿控系统设计的关键技术。
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