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.
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