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。
The designed maneuver reentry trajectory can meet the demands of attitude, heat flux and velocity for the warhead.
机动弹头是复杂的非线性系统，它给姿态控制系统设计人员以极大的挑战。
Maneuverable warhead are the complex nonlinear system, which take a great challenge to the attitude control system designers.
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。
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。
In view of the particularity for maneuver warhead reentry trajectory and the guidance method, key techniques in attitude control system design are analyzed.
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