$Rigid spacecraft nonlinear robust $$H_\infty $$ attitude controller design under actuator misalignments$

Rigid spacecraft nonlinear robust $$H_\infty $$ attitude controller design under actuator misalignments

Bibliographic Details
Published in:	Nonlinear dynamics. - Springer Netherlands, 1990. - 111(2023), 16 vom: 29. Juni, Seite 15037-15054
Main Author:	Wang, Zhong (Author)
Other Authors:	Li, Yan (Author)
Format:	electronic Article
Language:	English
Published:	2023
ISSN:	1573-269X
External Sources:	lizenzpflichtig

External Sources: lizenzpflichtig