Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control system, systematically and comprehensively presenting recent research results of fast maneuver attitude control for agile satellites by using advanced nonlinear control techniques. This reference book focuses on modelling and attitude control considering different actuator combinations, actuator installation deviation, actuator fault, and flexible appendage coupling effect for agile satellites, intended to provide a unified platform for understanding and applicability of agile satellites fast maneuverer and stabilization control for different purposes. This book will be an excellent resource for researchers working on spacecraft design; nonlinear control systems; vehicle systems; and complex control systems. Unifies existing and emerging concepts concerning nonlinear control theory, fault tolerant, and attitude control for agile satellites Provides a series of latest results in, including but not limited to, fast maneuverer and stabilization control, hybrid actuator control, nonlinear attitude control, fault tolerant control, and active vibration suppression towards agile satellites Comprehensively captures recent advances of theory, technological aspects, and applications of fast maneuverer and stabilization control in agile satellites Addresses research problems in each chapter. Numerical and simulation results are given in each chapter to reflect the engineering practice, yet demonstrate the focus of the developed analysis and synthesis approaches Contains comprehensive and up-to-date references, which plays an indicative role for further study of the readers INDICE: 1. Introduction and Literature Review2. Preliminaries and Mathematical Model3. Near Time-Optimal Control Based on Analytical Trajectory Planning4. Time Efficient Robust PID Plus Control with Constraints5. Bang-Bang Logic-based Time Efficient Sliding Mode Control6. Robust Finite Time Control Based on Three Stage Structure Sliding Mode7. Finite Time Output Feedback Attitude Control8. Observer-Based Continuous Finite-Time Attitude Control9. Neural Network-Based Finite Time Fault-Tolerant Attitude Control10. Hybrid Thrusters and Reaction Wheels based Attitude Control with High Precision11. Finite Time Attitude Control with Hybrid Actuators12. A Control Allocation Approach for Hybrid Actuator13. Conclusions and Future Works
- ISBN: 978-0-323-95455-6
- Editorial: Academic Press
- Encuadernacion: Rústica
- Páginas: 318
- Fecha Publicación: 31/08/2022
- Nº Volúmenes: 1
- Idioma: Inglés