Trajectory Optimization and Guidance Methods for Mars Entry
Author: by Shuang Li (Author), Xu Liu (Author), Xiu-qiang Jiang (Author), Yu-ming Peng (Author) & 1 more
Publisher: Springer
Edition: 2024th
Publication Date: 2024-03-13
Language: English
Print Length: 307 pages
ISBN-10: 9819962811
ISBN-13: 9789819962815
Book Description
This book systematically investigates the Mars entry problem from the perspectives of deterministic optimization, uncertainty optimization, and guidance. Began with a detailed review of the robotic missions and human-scaled exploration plans to Mars, theories or concepts of optimal control, uncertainty quantification, robust optimization, model predictive control, sequential convex programming, and computational guidance are subsequently introduced. Correspondingly, this book presents a series of trajectory planning and guidance algorithms to improve the robustness, reliability, and safety of the Mars missions. Because the Mars entry problem is studied using advanced mathematics, including probability theory, optimization theory, and cybernetics, thus the book is primarily designed as a textbook for graduate students in aerospace engineering, aeronautics, and astronautics departments. Engineers and researchers may also use this book as a reference or tutorial to help with the modeling and simulation of the Mars entry problem due to its thorough simulations and analyses.
From the Back Cover
About the Author
Xu Liu received the B.S. and Ph.D. degrees in Guidance, Navigation, and Control from Nanjing University of Aeronautics and Astronautics, Nanjing, China, in 2017 and 2023, respectively. He is a Lecturer with the Department of Automation, Nanchang University, Nanchang, China. His research interests include the trajectory optimization, guidance, navigation, and control technologies of flight vehicles.
Xiuqiang Jiang received his Ph.D. degree from the Nanjing University of Aeronautics and Astronautics, China. He was a visiting scholar at the University of Arizona, USA, during 2017–2018. He is currently an associate professor at the Department of Flight Vehicle Control and Information Engineering, Sichuan University, China. His research interests include trajectory optimization, uncertainty quantification, and guidance technologies for spacecraft. He published 21 papers in authoritative aerospace journals, including Progress in Aerospace Sciences, Aerospace Science and Technology, Acta Astronautica, etc., and also served as the reviewer for 11 academic journals.
Yuming Peng received his M.S.E. degree from Nanjing University of Aeronautics and Astronautics in 2011 and his Ph.D. degree from Nanjing University in 2019. Since 2011, he has worked as an engineer and a senior engineer at the Shanghai Institute of Satellite Engineering, Shanghai, China. He worked as an engineer in Orbit Dynamics and Control for China’s first Mars probe, Tianwen 1.
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