타이틀 |
Transmission Zeros of Spacecraft Attitude Control System |
저자 |
Takashi KIDA, Isao YAMAGUCHI |
Keyword |
Spacecraft; large space structures; attitude control; transmission zeros |
URL |
http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01166.pdf?id=NALTR0001166 |
보고서번호 |
NAL TR-1166 |
발행년도 |
1992.6 |
출처 |
NAL (National Aerospace Laboratory of Japan) |
ABSTRACT |
The importance of evaluating the control performance and the robust stability in the frequency-domain is being widely recognized.A pair of poles and zeros is a candidate characterizing the model of the control system when it is described in the transfer matrix form.This paper studies poles and zeros of multi-input/multi-output spacecraft attitude control system.Some algebraic algorithms for obtaining them are derived,and their dynamical properties are clarified.Herein considered is the transmission zero,among many definitions of the multi-variable zeros. |