| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide an attitude control device of a space vehicle capable of effectively and surely executing the attitude change of the space vehicle by the control of a CMG with high reliability. <P>SOLUTION: The attitude controlling device of the space vehicle installed in the space vehicle and changing the attitude of the space vehicle by controlling the CMG1 has the orbit planning part 12 calculating the orbit planning of the rotating angle around the gimbal shaft of the CMG1 as the time function connecting rotating angles at a plurality of times within the time needed for the rotating angle to reach from the initial value to the final value based on the targeted attitude of the space vehicle and calculating the orbit planning of the attitude angle of the space vehicle by temporally integrating the attitude angle speed of the space vehicle obtained by using the orbit planning of the rotating angle when changing the attitude of the space vehicle and controls the CMG1 by feedbacking the current value of the attitude angle of the space vehicle and the current value of the rotating angle. <P>COPYRIGHT: (C)2012,JPO&INPIT |
