000 04081nam a22005655i 4500
001 978-981-99-6282-2
003 DE-He213
005 20251030111717.0
007 cr nn 008mamaa
008 240312s2024 si | s |||| 0|eng d
020 _a9789819962822
_9978-981-99-6282-2
024 7 _a10.1007/978-981-99-6282-2
_2doi
050 4 _aTL1-4050
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
072 7 _aTRP
_2thema
072 7 _aTTDS
_2thema
100 1 _aLi, Shuang.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_972883
245 1 0 _aTrajectory Optimization and Guidance Methods for Mars Entry
_h[electronic resource] /
_cby Shuang Li, Xu Liu, Xiu-qiang Jiang, Yu-ming Peng.
250 _a1st ed. 2024.
264 1 _aSingapore :
_bSpringer Nature Singapore :
_bImprint: Springer,
_c2024.
300 _aIX, 298 p. 121 illus., 111 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
505 0 _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.
520 _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.
650 0 _aAerospace engineering.
_966335
650 0 _aAstronautics.
_966336
650 0 _aMathematical statistics
_xData processing.
_964750
650 1 4 _aAerospace Technology and Astronautics.
_966339
650 2 4 _aStatistics and Computing.
_966446
700 1 _aLiu, Xu.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_972884
700 1 _aJiang, Xiu-qiang.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_972885
700 1 _aPeng, Yu-ming.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_972886
710 2 _aSpringerLink (Online service)
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9789819962815
776 0 8 _iPrinted edition:
_z9789819962839
776 0 8 _iPrinted edition:
_z9789819962846
856 4 0 _uhttps://doi.org/10.1007/978-981-99-6282-2
912 _aZDB-2-ENG
912 _aZDB-2-SXE
999 _c58271
_d58271