Spacecraft Modeling, Attitude Determination, and Control: Quaternion-Based Approach

Author:   Yaguang Yang
Publisher:   Taylor & Francis Ltd
ISBN:  

9780367780357


Pages:   340
Publication Date:   31 March 2021
Format:   Paperback
Availability:   In Print   Availability explained
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Spacecraft Modeling, Attitude Determination, and Control: Quaternion-Based Approach


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Author:   Yaguang Yang
Publisher:   Taylor & Francis Ltd
Imprint:   CRC Press
Weight:   0.625kg
ISBN:  

9780367780357


ISBN 10:   0367780356
Pages:   340
Publication Date:   31 March 2021
Audience:   College/higher education ,  General/trade ,  Tertiary & Higher Education ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   In Print   Availability explained
This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us.

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Reviews

This book provides a good and comprehensive overview of spacecraft attitude dynamics, determination and control, including advances in the quaternion-based approach, with application to practical problems such as coupled attitude and orbit control and model predictive optimal control with realistic actuators constraints. In conclusion, the book is a good and useful resource for researchers and research minded engineers wishing to develop a more detailed understanding of some of the latest advances in robust pole placement and model predictive control to spacecraft attitude control. The quaternion based approach is applied to practical attitude estimation and attitude control problems ranging from nadir pointing using reaction wheels or CMGs to momentum dumping using magnetic torquers and coupled attitude and orbit control for spacecraft docking. -- Nadjim Horri, Coventry University, The Aeronautical Journal, Oct 2020


This book provides a good and comprehensive overview of spacecraft attitude dynamics, determination and control, including advances in the quaternion-based approach, with application to practical problems such as coupled attitude and orbit control and model predictive optimal control with realistic actuators constraints. In conclusion, the book is a good and useful resource for researchers and research minded engineers wishing to develop a more detailed understanding of some of the latest advances in robust pole placement and model predictive control to spacecraft attitude control. The quaternion based approach is applied to practical attitude estimation and attitude control problems ranging from nadir pointing using reaction wheels or CMGs to momentum dumping using magnetic torquers and coupled attitude and orbit control for spacecraft docking. -- Nadjim Horri, Coventry University, The Aeronautical Journal, Oct 2020


Author Information

Yaguang Yang received his B.S. (1982) and M.S. (1985) degrees from Huazhong University of Science and Technology, China. From 1985 to 1990, he was a lecturer at Zhejiang University in China. In 1996 he received a PhD degree from the Department of Electrical and Computer Engineering at the University of Maryland, College Park. He designed and implemented control systems at UKIRT, CIENA, ITT, and Orbital Sciences Corporation. He is currently with the US Nuclear Regulatory Commission.

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