Spacecraft Attitude Control - A Linear Matrix Inequality Approach (Paperback)

Spacecraft Attitude Control: A Linear Matrix Inequality Approach solves problems for spacecraft attitude control systems using convex optimization and, specifi cally, 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. The authors describe a wide variety of novel and robust controllers, applicable both to spacecraft attitude control and easily extendable to second-order systems. Spacecraft Attitude Control provides its readers with an accessible introduction to spacecraft attitude control and robust systems, giving an extensive survey of current research and helping researchers improve robust control performance.

General

Imprint:	Elsevier - Health Sciences Division
Country of origin:	United States
Release date:	February 2022
First published:	2022
Authors:	Chuang Liu • Xiaokui Yue • Keke Shi • Zhaowei Sun
Dimensions:	229 x 152 x 25mm (L x W x T)
Format:	Paperback
Pages:	384
ISBN-13:	978-0-323-99005-9
Categories:	Books > Professional & Technical > Mechanical engineering & materials > Materials science > Mechanics of fluids > Aerodynamics Promotions
LSN:	0-323-99005-3
Barcode:	9780323990059

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