東華大學圖書館 |

Language: English

Help

回圖書館首頁

手機版館藏查詢

Back

Switch To: Labeled | MARC Mode | ISBD

Linked to FindBook

Google Book

Amazon

博客來

Trajectory optimization and guidance methods for Mars entry

Record Type:	Electronic resources : Monograph/item
Title/Author:	Trajectory optimization and guidance methods for Mars entry/ by Shuang Li ... [et al.].
other author:	Li, Shuang.
Published:	Singapore :Springer Nature Singapore : : 2024.,
Description:	ix, 298 p. :ill. (chiefly col.), digital ;24 cm.
[NT 15003449]:	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.
Contained By:	Springer Nature eBook
Subject:	Space vehicles - Atmospheric entry - Mars (Planet) -
Online resource:	https://doi.org/10.1007/978-981-99-6282-2
ISBN:	9789819962822

Trajectory optimization and guidance methods for Mars entry
Trajectory optimization and guidance methods for Mars entry[electronic resource] /by Shuang Li ... [et al.]. - Singapore :Springer Nature Singapore :2024. - ix, 298 p. :ill. (chiefly col.), digital ;24 cm.

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.

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.

ISBN: 9789819962822

Standard No.: 10.1007/978-981-99-6282-2doiSubjects--Topical Terms:

3715302
Space vehicles
--Atmospheric entry--Mars (Planet)

LC Class. No.: TL1060

Dewey Class. No.: 629.415

Trajectory optimization and guidance methods for Mars entry
LDR:02946nmm a22003495a 4500 001 2370160
003 DE-He213
005 20240312131931.0
006 m d
007 cr nn 008maaau
008 241127s2024 si s 0 eng d
020 $a 9789819962822 $q (electronic bk.)
020 $a 9789819962815 $q (paper)
024 7 $a 10.1007/978-981-99-6282-2 $2 doi
035 $a 978-981-99-6282-2
040 $a GP $c GP
041 0 $a eng
050 4 $a TL1060
072 7 $a TRP $2 bicssc
072 7 $a TTDS $2 bicssc
072 7 $a TEC002000 $2 bisacsh
072 7 $a TRP $2 thema
072 7 $a TTDS $2 thema
082 0 4 $a 629.415 $2 23
090 $a TL1060 $b .T768 2024
245 0 0 $a Trajectory optimization and guidance methods for Mars entry $h [electronic resource] / $c by Shuang Li ... [et al.].
260 $a Singapore : $b Springer Nature Singapore : $b Imprint: Springer, $c 2024.
300 $a ix, 298 p. : $b ill. (chiefly col.), digital ; $c 24 cm.
505 0 $a 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.
520 $a 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.
650 0 $a Space vehicles $x Atmospheric entry $z Mars (Planet) $3 3715302
650 1 4 $a Aerospace Technology and Astronautics. $3 928116
650 2 4 $a Statistics and Computing. $3 3594429
700 1 $a Li, Shuang. $3 3715301
710 2 $a SpringerLink (Online service) $3 836513
773 0 $t Springer Nature eBook
856 4 0 $u https://doi.org/10.1007/978-981-99-6282-2
950 $a Engineering (SpringerNature-11647)