When the number of CMGs is represented by n (n is an integer of 4 or more), (n−3) gimbal angles out of n gimbal angles corresponding to the n CMGs are set as free parameters, and an algebraic equation representing a relationship among three gimbal angles out of the n gimbal angles, the free parameters, and an angular momentum of all the CMGs is used to solve the algebraic equation while changing the free parameters within set ranges, to thereby obtain solutions of the gimbal angles of the plurality of CMGs required for achieving a given angular momentum.
Device for controlling attitude of spacecraft and method for calculating CMG gimbal angle
2019-09-10
Patent
Electronic Resource
English
DEVICE FOR CONTROLLING ATTITUDE OF SPACECRAFT AND METHOD FOR CALCULATING CMG GIMBAL ANGLE
European Patent Office | 2019
|DEVICE FOR CONTROLLING ATTITUDE OF SPACECRAFT AND METHOD FOR CALCULATING CMG GIMBAL ANGLE
European Patent Office | 2019
|DEVICE FOR CONTROLLING ATTITUDE OF SPACECRAFT AND METHOD FOR CALCULATING CMG GIMBAL ANGLE
European Patent Office | 2016
|Spacecraft attitude maneuver using two single-gimbal control moment gyros
Online Contents | 2013
|