國立虎尾科技大學 |

Steady Glide Dynamics and Guidance of Hypersonic Vehicle

Record Type:	Language materials, printed : Monograph/item
Title/Author:	Steady Glide Dynamics and Guidance of Hypersonic Vehicle/ by Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang.
Author:	Chen, Wanchun.
other author:	Zhou, Hao.
Description:	XXXII, 461 p. 318 illus., 97 illus. in color.online resource. :
Contained By:	Springer Nature eBook
Subject:	Aerospace engineering. -
Online resource:	https://doi.org/10.1007/978-981-15-8901-0
ISBN:	9789811589010

Steady Glide Dynamics and Guidance of Hypersonic Vehicle
Chen, Wanchun.

Steady Glide Dynamics and Guidance of Hypersonic Vehicle[electronic resource] /by Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang. - 1st ed. 2021. - XXXII, 461 p. 318 illus., 97 illus. in color.online resource.

Introduction -- Mathematical Fundamentals -- The Mathematical Model for Hypersonic Entry Glide Vehicle -- Mathematical description of optimal control problem for entry gliding -- Indirect approch to the optimal glide trajectory problem -- Direct Method for Gliding Trajectory Optimization Problem -- The Concept of Steady Glide Reentry Trajectory and the Stability of its Regular Perturbation Solutions -- Analytical Solutions of Steady Glide Reentry Trajectory in Three Dimensions and their Application to Trajectory Planning -- Trajectory Damping Control Technique for Hypersonic Glide Reentry -- Steady Glide Dynamic Modeling and Trajectory Optimization for High Lift-to-Drag Ratio Reentry Vehicle -- Singular Perturbation Guidance of Hypersonic Glide Reentry -- 3-D Reentry Guidance with Real-Time Planning of Reference with New Analytical Solutions Based on Spectral Decomposition Method -- Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical glide Formulas with the Consideration of the effects of the Earth's rotation -- Analytical Entry Guidance based on Steady Glide -- Linear Pseudospectral General Nominal Effort Miss Distance Guidance Method -- Linear Pseudospectral Adaptive Flight Phase Segmentation General Nominal Effort Miss Distance Reentry Guidance -- Trajectory-Shaping Guidance with Final Speed and Load Factor Constraints.

This book presents the latest researches on hypersonic steady glide dynamics and guidance, including the concept of steady glide reentry trajectory and the stability of its regular perturbation solutions, trajectory damping control technique for hypersonic glide reentry, singular perturbation guidance of hypersonic glide reentry, trajectory optimization based on steady glide, linear pseudospectral generalized nominal effort miss distance guidance, analytical entry guidance and trajectory-shaping guidance with final speed and load factor constraints. They can be used to solve many new difficult problems in entry guidance. And many practical engineering cases are provided for the readers for better understanding. Researchers and students in the fields of flight vehicle design or flight dynamics, guidance and control could use the book as valuable reference.

ISBN: 9789811589010

Standard No.: 10.1007/978-981-15-8901-0doiSubjects--Topical Terms:

686400
Aerospace engineering.

LC Class. No.: TL787-4050.22

Dewey Class. No.: 629.1

Steady Glide Dynamics and Guidance of Hypersonic Vehicle
LDR:03641nam a22004215i 4500 001 1048368
003 DE-He213
005 20210622094807.0
007 cr nn 008mamaa
008 220103s2021 si | s |||| 0|eng d
020 $a 9789811589010 $9 978-981-15-8901-0
024 7 $a 10.1007/978-981-15-8901-0 $2 doi
035 $a 978-981-15-8901-0
050 4 $a TL787-4050.22
050 4 $a TC1-1800
072 7 $a TRP $2 bicssc
072 7 $a TEC002000 $2 bisacsh
072 7 $a TRP $2 thema
072 7 $a TTDS $2 thema
082 0 4 $a 629.1 $2 23
100 1 $a Chen, Wanchun. $e author. $4 aut $4 http://id.loc.gov/vocabulary/relators/aut $3 1352224
245 1 0 $a Steady Glide Dynamics and Guidance of Hypersonic Vehicle $h [electronic resource] / $c by Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang.
250 $a 1st ed. 2021.
264 1 $a Singapore : $b Springer Singapore : $b Imprint: Springer, $c 2021.
300 $a XXXII, 461 p. 318 illus., 97 illus. in color. $b online resource.
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
347 $a text file $b PDF $2 rda
505 0 $a Introduction -- Mathematical Fundamentals -- The Mathematical Model for Hypersonic Entry Glide Vehicle -- Mathematical description of optimal control problem for entry gliding -- Indirect approch to the optimal glide trajectory problem -- Direct Method for Gliding Trajectory Optimization Problem -- The Concept of Steady Glide Reentry Trajectory and the Stability of its Regular Perturbation Solutions -- Analytical Solutions of Steady Glide Reentry Trajectory in Three Dimensions and their Application to Trajectory Planning -- Trajectory Damping Control Technique for Hypersonic Glide Reentry -- Steady Glide Dynamic Modeling and Trajectory Optimization for High Lift-to-Drag Ratio Reentry Vehicle -- Singular Perturbation Guidance of Hypersonic Glide Reentry -- 3-D Reentry Guidance with Real-Time Planning of Reference with New Analytical Solutions Based on Spectral Decomposition Method -- Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical glide Formulas with the Consideration of the effects of the Earth's rotation -- Analytical Entry Guidance based on Steady Glide -- Linear Pseudospectral General Nominal Effort Miss Distance Guidance Method -- Linear Pseudospectral Adaptive Flight Phase Segmentation General Nominal Effort Miss Distance Reentry Guidance -- Trajectory-Shaping Guidance with Final Speed and Load Factor Constraints.
520 $a This book presents the latest researches on hypersonic steady glide dynamics and guidance, including the concept of steady glide reentry trajectory and the stability of its regular perturbation solutions, trajectory damping control technique for hypersonic glide reentry, singular perturbation guidance of hypersonic glide reentry, trajectory optimization based on steady glide, linear pseudospectral generalized nominal effort miss distance guidance, analytical entry guidance and trajectory-shaping guidance with final speed and load factor constraints. They can be used to solve many new difficult problems in entry guidance. And many practical engineering cases are provided for the readers for better understanding. Researchers and students in the fields of flight vehicle design or flight dynamics, guidance and control could use the book as valuable reference.
650 0 $a Aerospace engineering. $3 686400
650 0 $a Astronautics. $3 646219
650 0 $a Control engineering. $3 1249728
650 0 $a Astronomy. $3 593935
650 0 $a Astrophysics. $3 646223
650 0 $a Mathematical optimization. $3 527675
650 0 $a System theory. $3 566168
650 1 4 $a Aerospace Technology and Astronautics. $3 683885
650 2 4 $a Control and Systems Theory. $3 1211358
650 2 4 $a Astronomy, Astrophysics and Cosmology. $3 593936
650 2 4 $a Optimization. $3 669174
650 2 4 $a Systems Theory, Control. $3 669337
700 1 $a Zhou, Hao. $e editor. $4 aut $4 http://id.loc.gov/vocabulary/relators/aut $3 1283345
700 1 $a Yu, Wenbin. $e author. $4 aut $4 http://id.loc.gov/vocabulary/relators/aut $3 1352225
700 1 $a Yang, Liang. $e author. $4 aut $4 http://id.loc.gov/vocabulary/relators/aut $3 1352226
710 2 $a SpringerLink (Online service) $3 593884
773 0 $t Springer Nature eBook
776 0 8 $i Printed edition: $z 9789811589003
776 0 8 $i Printed edition: $z 9789811589027
776 0 8 $i Printed edition: $z 9789811589034
856 4 0 $u https://doi.org/10.1007/978-981-15-8901-0
912 $a ZDB-2-ENG
912 $a ZDB-2-SXE
950 $a Engineering (SpringerNature-11647)
950 $a Engineering (R0) (SpringerNature-43712)