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:
Online Access:Connect to the full text of this electronic book
Description
Summary:"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 disturbances and other uncertainties are requirements for the current generation of spacecraft. This book presents an LMI approach to spacecraft attitude control and shows that all uncertainties in the maneuvering process can be solved numerically. It explains how a model-like state space can be developed through a mathematical presentation of attitude control systems, allowing the controller in question to be applied universally."--
Physical Description:1 online resource (1 volume)
ISBN:0323990061
9780323990066