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MANIPULATION METHOD SUITABLE FOR NON-REDUNDANT SGCMG GROUP

机译:适用于非冗余SGCMG组的操作方法

摘要

A manipulation method suitable for a non-redundant SGCMG group. The method comprises the steps: 1) determining, according to configurations and synthetic angular momentums of n SGCMGs, nominal frame angle vectors of the configurations of n SGCMGs, wherein n ≥ 3; 2) determining, according to a frame angle of each SGCMG, Jacob of a motion equation of the frame angle and the deviation of the frame angle from a nominal value; and 3) determining, according to the Jacob and the deviation of the frame angle from the nominal value that are determined in step 2), a frame angular velocity instruction of the SGCMG. According to the method of the present invention, the distance that a frame angle is deviated from the nominal value, a frame angle instruction amplitude value, and a torque output deviation are taken into consideration, such that the capability of avoiding singularities in attitude maneuvering and returning to a frame nominal position after maneuvering is achieved, the contradiction between singularity avoidance and an attitude control torque of a CMG frame is resolved, and the realization of high performance of maneuvering along any attitude can be ensured.
机译:一种适用于非冗余SGCMG组的操作方法。该方法包括步骤:1)确定,根据N SGCMG的构造和合成角动量,n SGCMG的配置的标称框架角度向量,其中n≥3; 2)根据每个SGCMG的帧角度确定,帧角度的运动方程的jacob与帧角度与标称值的偏差; 3)根据Jacob确定,根据步骤2中确定的标称值的帧角度和帧角度的偏差,SGCMG的帧角速度指令。根据本发明的方法,考虑帧角度偏离帧角度,帧角度指令幅度值和扭矩输出偏差的距离,使得避免姿态操纵和操纵奇迹的能力在实现操纵之后返回框架标称位置,解决了CMG帧的奇异性避免和姿态控制扭矩的矛盾,并且可以确保沿任何姿态进行高性能的实现。

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