Fast Satellite Attitude Maneuver and Control

Häftad, Engelska, 2022

Del i serien Emerging Methodologies and Applications in Modelling, Identification and Control

1 540 kr

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Beskrivning

Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control systems, 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 modeling and attitude control, considering different actuator combinations, actuator installation deviation, actuator fault, and flexible appendage coupling effect for agile satellites. The book provides a unified platform for understanding and applicability of agile satellites fast maneuverer and stabilization control for different purposes.

It 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 the latest results, 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, along with numerical and simulation results that reflect engineering practice and demonstrate the focus of developed analysis and synthesis approaches
Contains comprehensive, up-to-date references, which play an indicative role for further study

Produktinformation

Utgivningsdatum:2022-08-03
Mått:152 x 229 x 19 mm
Vikt:450 g
Format:Häftad
Språk:Engelska
Serie:Emerging Methodologies and Applications in Modelling, Identification and Control
Antal sidor:278
Förlag:Elsevier Science
ISBN:9780323954556

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Maskinteknik och material inom Naturvetenskap och teknik

Mer om författaren

Dong Ye is a Professor at the School of Astronautics, Harbin Institute, in China. His research interests include spacecraft dynamics and control and hardware-in-the-loop simulation technique. You Li graduated from Harbin Institute of Technology in 2017, and now is a Lecturer at the School of Aerospace Science and Technology, Xidian University, in China. His work is mainly focusing on satellite attitude control, especially on satellite attitude fast maneuver. Yan Xiao received his Ph.D. degree in Aeronautical and Astronautical Science and Technology from the Harbin Institute of Technology (HIT) and now is an Assistant Professor at the School of Astronautics, HIT. His current research interests include nonlinear control, spacecraft attitude dynamics and control, coordination control, etc.

Innehållsförteckning

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