LEADER 03632nam 22005415 450 001 9910842489903321 005 20240312131931.0 010 $a981-9962-82-X 024 7 $a10.1007/978-981-99-6282-2 035 $a(MiAaPQ)EBC31209896 035 $a(Au-PeEL)EBL31209896 035 $a(DE-He213)978-981-99-6282-2 035 $a(EXLCZ)9930892382400041 100 $a20240312d2024 u| 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aTrajectory Optimization and Guidance Methods for Mars Entry$b[electronic resource] /$fby Shuang Li, Xu Liu, Xiu-qiang Jiang, Yu-ming Peng 205 $a1st ed. 2024. 210 1$aSingapore :$cSpringer Nature Singapore :$cImprint: Springer,$d2024. 215 $a1 online resource (297 pages) 311 $a981-9962-81-1 327 $aFundamental 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. 330 $aThis 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. 606 $aAerospace engineering 606 $aAstronautics 606 $aMathematical statistics$xData processing 606 $aAerospace Technology and Astronautics 606 $aStatistics and Computing 615 0$aAerospace engineering. 615 0$aAstronautics. 615 0$aMathematical statistics$xData processing. 615 14$aAerospace Technology and Astronautics. 615 24$aStatistics and Computing. 676 $a629.411 700 $aLi$b Shuang$01733081 701 $aLiu$b Xu$0953796 701 $aJiang$b Xiu-qiang$01733082 701 $aPeng$b Yu-ming$01733083 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910842489903321 996 $aTrajectory Optimization and Guidance Methods for Mars Entry$94148126 997 $aUNINA