Spacecraft attitude control : a linear matrix inequality approach /

"Spacecraft Attitude Control: A Linear Matrix Inequality Approach solves problems for spacecraft attitude control systems using convex optimization and, specifically, through a linear matrix inequality (LMI) approach. High-precision pointing and improved robustness in the face of external distu...

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Bibliographic Details

Main Authors:	Liu, Chuang (Author), Yue, Xiaokui (Author), Shi, Keke (Author), Sun, Zhaowei (Author)
Corporate Author:	ScienceDirect (Online service)
Format:	eBook
Language:	English
Published:	Amsterdam : Elsevier, 2022.
Subjects:	Space vehicles > Attitude control systems. Véhicules spatiaux > Systèmes de commande d'orientation. Space vehicles > Attitude control systems Electronic books.
Online Access:	Connect to the full text of this electronic book