Li, Shuang. creator author. aut http://id.loc.gov/vocabulary/relators/aut Liu, Xu. author. aut http://id.loc.gov/vocabulary/relators/aut Jiang, Xiu-qiang. author. aut http://id.loc.gov/vocabulary/relators/aut Peng, Yu-ming. author. aut http://id.loc.gov/vocabulary/relators/aut SpringerLink (Online service) text si 2024 1st ed. 2024. monographic eng

electronic

electronic resource

access IX, 298 p. 121 illus., 111 illus. in color. online resource. 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. Fundamental Knowledge -- Introduction -- Preliminaries -- Deterministic Optimization -- Improved Gauss pseudospectral method for Mars entry trajectory planning -- Improved sequential convex optimization for Mars entry trajectory planning -- Pseudospectral model predictive convex programming for Mars entry trajectory planning -- Indirect sequential convex programming for Mars entry trajectory planning -- Mars entry and powered descent using collaborative optimization -- Uncertainty optimization -- Mars entry trajectory optimization with desensitized optimal control -- Uncertainty quantification for Mars entry -- Robust trajectory optimization for Mars entry -- Robust optimal guidance method -- Direct model reference adaptive tracking guidance for Mars entry -- Computational guidance method for Mars entry. by Shuang Li, Xu Liu, Xiu-qiang Jiang, Yu-ming Peng. Aerospace engineering Astronautics Mathematical statistics Data processing Aerospace Technology and Astronautics Statistics and Computing TL1-4050 9789819962822 https://doi.org/10.1007/978-981-99-6282-2 https://doi.org/10.1007/978-981-99-6282-2 240312 20251030111717.0 978-981-99-6282-2