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METHOD OF COMMANDING AN ATTITUDE CONTROL SYSTEM AND ATTITUDE CONTROL SYSTEM OF A SPACE VEHICLE

机译:一种空间车辆的姿态控制系统和姿态控制系统的方法

摘要

A method for controlling an attitude control system (30) for a space vehicle (10), the attitude of the space vehicle being controlled during at least one preparation phase followed by an observation phase during which an image capture is performed. In an attitude control system that includes a maneuvering subsystem (300) which includes at least one reaction wheel, the method includes, during the at least one preparation phase, a preparation step (50), during which commands are issued to the maneuvering subsystem in order to control the attitude of the space vehicle, followed by a step (55) of stopping the at least one reaction wheel prior to the observation phase. In addition, during the observation phase, a fine control subsystem (310) having a lower vibration signature than that of the maneuvering subsystem, is sent commands in order to control the space vehicle's attitude. An attitude control system for a space vehicle is also described.
机译:一种用于控制航天器(10)的姿态控制系统(30)的方法,该航天器的姿态在至少一个准备阶段,随后是进行图像捕获的观察阶段期间被控制。在包括操纵子系统(300)的姿态控制系统中,该操纵子系统包括至少一个反作用轮,该方法包括在至少一个准备阶段期间的准备步骤(50),在该步骤中,命令被发送到操纵子系统。为了控制航天器的姿态,随后是在观察阶段之前停止至少一个反作用轮的步骤(55)。另外,在观察阶段期间,向振动控制信号低于操纵子系统的精细控制子系统(310)发送命令,以控制航天器的姿态。还描述了用于航天器的姿态控制系统。

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