Spacecraft reentrytrajectory 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。
2
The designed maneuver reentrytrajectory 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。
3
In view of the particularity for maneuver warhead reentrytrajectory and the guidance method, key techniques in attitude control system design are analyzed.