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首页> 外文期刊>日本航空宇宙学会論文集 >DESIGN OF ATTITUDE CONTROL SYSTEM FOR SPINNING VEHICLE BY COMBINATION OF ONE-SHOT THRUSTERS
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DESIGN OF ATTITUDE CONTROL SYSTEM FOR SPINNING VEHICLE BY COMBINATION OF ONE-SHOT THRUSTERS

机译:组合式一键推力车姿态控制系统设计。

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摘要

The main feature of one-shot thrusters is discreteness in both time and space domain. We apply discrete-time sliding mode control to the attitude control of a spinning vehicle. And we consider the space discreteness by applying a simple selection algorithm (SSA) to the selection of the combination of one-shot thrusters prearranged on the vehicle in order to generate the control force. SSA is the new algorithm we proposed, and its calculation load is light in computation load. We adopt a regulator scheme to reject disturbances of precession for precession for a LUNAR-A type penetrator , and conduct numerical simulations of the problem to show the effectiveness of the proposed control algorithm for one-shot thrusters.
机译:单发推进器的主要特征是时域和空域的离散性。我们将离散时间滑模控制应用于旋转车的姿态控制。并且我们通过将简单选择算法(SSA)应用于在车辆上预先布置的单发推进器组合的选择中以产生控制力来考虑空间离散性。 SSA是我们提出的新算法,其计算量很小。我们采用一种调节器方案来拒绝LUNAR-A型穿透器进动的进动干扰,并对该问题进行数值模拟,以显示所提出的单发推进器控制算法的有效性。

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