On the ground of developing the shuttle entry attitude simulation systems,this paper presents the minimum energy and time control logic for the case of multifarious disturbance torques.

• 以航天飞机再入姿态气浮台仿真控制系统的研制为背景,研究了气浮台在具有各种扰动的情况下,既能维持台体姿态又能保证时间推进剂控制点火逻辑问题。