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Control System and Control Method for Controlling a Momentum Wheel Device for Stabilizing a Spacecraft

机译:用于控制稳定宇宙飞船动量轮装置的控制系统及控制方法

摘要

A control system for a momentum wheel device is specified, wherein the momentum wheel device is a real momentum wheel device (1) and has a momentum wheel which is driven by a motor, and wherein a simulated momentum wheel device (2) is provided which simulates the behaviour of an ideal momentum wheel on the basis of an ideal physical model (12). The rotational speed of both the real momentum wheel device (1) and of the simulated momentum wheel device (2) can be changed by a torque command (6). A comparator device (11) is provided for comparing the real rotational angle (9) of the real momentum wheel device (1) and the simulated rotational angle (14) of the simulated momentum wheel device (2) and for generating a fault signal (15) corresponding to a deviation between the real rotational angle (9) and the simulated rotational angle (14). The fault signal (15) can be conducted to a control device (3), in order to actuate the motor on the basis of the fault signal (15), for the purpose of reducing the deviation.
机译:指定了用于动量轮装置的控制系统,其中,动量轮装置是真正的动量轮装置( 1 )模拟理想动量轮的行为的装置( 2 )。真正的动量轮装置( 1 )和模拟动量轮装置( 2 )的旋转速度可以通过扭矩命令改变( 6 < / b>)。提供比较器装置( 11 ),用于比较真实动量轮装置( 1 )和模拟的真实旋转角度( 9 )和模拟模拟动量轮装置( 2 )的旋转角度( 14 ),并用于产生对应于之间的偏差的故障信号( 15 )实际旋转角度( 9 )和模拟旋转角度( 14 )。故障信号( 15 )可以传导到控制装置( 3 ),以便基于故障信号( 15 < / b>),为了降低偏差。

著录项

  • 公开/公告号US2021171222A1

    专利类型

  • 公开/公告日2021-06-10

    原文格式PDF

  • 申请/专利权人 ROCKWELL COLLINS DEUTSCHLAND GMBH;

    申请/专利号US201917264121

  • 发明设计人 MARKUS EHINGER;

    申请日2019-07-04

  • 分类号B64G1/28;

  • 国家 US

  • 入库时间 2022-08-24 19:08:12

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