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    • 6. 发明申请
    • SYSTEM AND METHOD FOR ATTITUDE CONTROL AND STATION KEEPING
    • 用于姿态控制和站保持的系统和方法
    • US20050001102A1
    • 2005-01-06
    • US10710004
    • 2004-06-11
    • Peter Schubert
    • Peter Schubert
    • B64G1/24B64G1/26B64G1/36
    • B64G1/26B64G1/242B64G1/36
    • A system and method for supplying thrust to a structure, such as a satellite or spacecraft, for the purposes of station keeping and attitude control of the structure in low-gravity (orbital) and zero-gravity environments. The system includes devices for emitting energy beams and targets impacted by the energy beams to cause ablation of the targets. The beam-emitting devices and targets are adapted to cooperate and cause the structure to selectively undergo translational and/or rotational motion in reaction to the motion of material ablated from the targets. The position, alignment, and/or attitude of the structure can thereby be controlled in a zero or low-gravity environment by selectively emitting the energy beams at the targets.
    • 为了在低重力(轨道)和零重力环境下的结构的站保持和姿态控制的目的,向诸如卫星或航天器的结构提供推力的系统和方法。 该系统包括用于发射能量束和受能量束影响的靶的装置,以引起目标的消融。 射束发射装置和目标适于协调并使得结构选择性地进行平移和/或旋转运动,以反应从目标消融的材料的运动。 因此,可以通过选择性地在目标处发射能量束,在零或低重力环境中控制结构的位置,对准和/或姿态。