パラメータ変動のある宇宙構造物の制御 : ディスクリプタ形式によるμ設計

概要

論文の詳細を見る
This paper describes the attitude control problem of a flexible parameter varying spacecraft. Considered herein is the spacecraft consists of the main rigid body and some flexible solar paddles which rotate at the orbital rate in order to generate more electricity. In this case, the interference characteristics of the elastic vibration of the paddles and the attitude motion of the body changes depending on the paddle angie. Therefore, the attitude control system of such spacecraft becomes parameter varying. This paper is intended to establish the systematic robust control synthesis procedure for this problem by applying fixed controller via μ synthesis. Capability of the methed is investigated by the numerical study using the model of the ETS-VI spacecraft.
一般社団法人日本機械学会の論文
1999-07-25