Language:
English
繁體中文
Help
圖資館首頁
Login
Back
Switch To:
Labeled
|
MARC Mode
|
ISBD
Optimal guidance and its application...
~
He, Shaoming.
Optimal guidance and its applications in missiles and UAVs
Record Type:
Electronic resources : Monograph/item
Title/Author:
Optimal guidance and its applications in missiles and UAVsby Shaoming He ... [et al.].
other author:
He, Shaoming.
Published:
Cham :Springer International Publishing :2020.
Description:
xiii, 214 p. :ill., digital ;24 cm.
Contained By:
Springer eBooks
Subject:
Guided missilesGuidance systems.
Online resource:
https://doi.org/10.1007/978-3-030-47348-8
ISBN:
9783030473488$q(electronic bk.)
Optimal guidance and its applications in missiles and UAVs
Optimal guidance and its applications in missiles and UAVs
[electronic resource] /by Shaoming He ... [et al.]. - Cham :Springer International Publishing :2020. - xiii, 214 p. :ill., digital ;24 cm. - Springer aerospace technology,1869-1730. - Springer aerospace technology..
Introduction of Optimal Guidance -- Optimality of Error Dynamics in Missile Guidance -- Three-Dimensional Optimal Impact-Time-Control Guidance Law -- Gravity-Turn Assisted Optimal Guidance Law -- Observability-Enhancement Optimal Guidance Law -- Optimal Proportional-Integral Guidance Law -- Energy-Optimal Waypoint-Following Guidance Law -- Conclusions.
This book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority.
ISBN: 9783030473488$q(electronic bk.)
Standard No.: 10.1007/978-3-030-47348-8doiSubjects--Topical Terms:
743403
Guided missiles
--Guidance systems.
LC Class. No.: UG630
Dewey Class. No.: 623.4519
Optimal guidance and its applications in missiles and UAVs
LDR
:02338nmm a2200349 a 4500
001
579680
003
DE-He213
005
20200928112514.0
006
m
007
cr
008
201229s2020
020
$a
9783030473488$q(electronic bk.)
020
$a
9783030473471$q(paper)
024
7
$a
10.1007/978-3-030-47348-8
$2
doi
035
$a
978-3-030-47348-8
040
$a
GP
$c
GP
041
0
$a
eng
050
4
$a
UG630
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
623.4519
$2
23
090
$a
UG630
$b
.O62 2020
245
0 0
$a
Optimal guidance and its applications in missiles and UAVs
$h
[electronic resource] /
$c
by Shaoming He ... [et al.].
260
$a
Cham :
$b
Springer International Publishing :
$b
Imprint: Springer,
$c
2020.
300
$a
xiii, 214 p. :
$b
ill., digital ;
$c
24 cm.
490
1
$a
Springer aerospace technology,
$x
1869-1730
505
0
$a
Introduction of Optimal Guidance -- Optimality of Error Dynamics in Missile Guidance -- Three-Dimensional Optimal Impact-Time-Control Guidance Law -- Gravity-Turn Assisted Optimal Guidance Law -- Observability-Enhancement Optimal Guidance Law -- Optimal Proportional-Integral Guidance Law -- Energy-Optimal Waypoint-Following Guidance Law -- Conclusions.
520
$a
This book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority.
650
0
$a
Guided missiles
$x
Guidance systems.
$3
743403
650
0
$a
Drone aircraft
$x
Control systems.
$3
492279
650
1 4
$a
Aerospace Technology and Astronautics.
$3
309707
650
2 4
$a
Control, Robotics, Mechatronics.
$3
339147
650
2 4
$a
Computational Intelligence.
$3
338479
700
1
$a
He, Shaoming.
$3
869108
710
2
$a
SpringerLink (Online service)
$3
273601
773
0
$t
Springer eBooks
830
0
$a
Springer aerospace technology.
$3
558627
856
4 0
$u
https://doi.org/10.1007/978-3-030-47348-8
950
$a
Engineering (Springer-11647)
based on 0 review(s)
ALL
電子館藏
Items
1 records • Pages 1 •
1
Inventory Number
Location Name
Item Class
Material type
Call number
Usage Class
Loan Status
No. of reservations
Opac note
Attachments
000000184266
電子館藏
1圖書
電子書
EB UG630 .O62 2020 2020
一般使用(Normal)
On shelf
0
1 records • Pages 1 •
1
Multimedia
Multimedia file
https://doi.org/10.1007/978-3-030-47348-8
Reviews
Add a review
and share your thoughts with other readers
Export
pickup library
Processing
...
Change password
Login