Language:
English
繁體中文
Help
Login
Back
Switch To:
Labeled
|
MARC Mode
|
ISBD
Flexible Spacecraft Dynamics, Contro...
~
Mazzini, Leonardo.
Flexible Spacecraft Dynamics, Control and Guidance = Technologies by Giovanni Campolo /
Record Type:
Language materials, printed : Monograph/item
Title/Author:
Flexible Spacecraft Dynamics, Control and Guidance/ by Leonardo Mazzini.
Reminder of title:
Technologies by Giovanni Campolo /
Author:
Mazzini, Leonardo.
Description:
XXI, 363 p.online resource. :
Contained By:
Springer Nature eBook
Subject:
Aerospace engineering. -
Online resource:
https://doi.org/10.1007/978-3-319-25540-8
ISBN:
9783319255408
Flexible Spacecraft Dynamics, Control and Guidance = Technologies by Giovanni Campolo /
Mazzini, Leonardo.
Flexible Spacecraft Dynamics, Control and Guidance
Technologies by Giovanni Campolo /[electronic resource] :by Leonardo Mazzini. - 1st ed. 2016. - XXI, 363 p.online resource. - Springer Aerospace Technology,1869-1730. - Springer Aerospace Technology,.
Introduction -- The Kinematic of the flexible satellite -- The Satellite Attitude Control System -- The Dynamic of the flexible body -- The Dynamic in the Gravitational Field -- The Optimal Control Theory -- Attitude Control Methods -- Orbital Dynamic and Control -- Spacecraft Propulsion -- Sensors and Actuators technologies -- Complements to Body Kinematic -- Elements of Estimation Theory -- Basics of Lagrangian Equations -- The J2 perturbation solution -- Complements to Optimal Orbital Transfer -- Elements of Plasma physics.
This book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators.
ISBN: 9783319255408
Standard No.: 10.1007/978-3-319-25540-8doiSubjects--Topical Terms:
686400
Aerospace engineering.
LC Class. No.: TL787-4050.22
Dewey Class. No.: 629.1
Flexible Spacecraft Dynamics, Control and Guidance = Technologies by Giovanni Campolo /
LDR
:03022nam a22004335i 4500
001
979654
003
DE-He213
005
20200703120950.0
007
cr nn 008mamaa
008
201211s2016 gw | s |||| 0|eng d
020
$a
9783319255408
$9
978-3-319-25540-8
024
7
$a
10.1007/978-3-319-25540-8
$2
doi
035
$a
978-3-319-25540-8
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
Mazzini, Leonardo.
$4
aut
$4
http://id.loc.gov/vocabulary/relators/aut
$3
1102778
245
1 0
$a
Flexible Spacecraft Dynamics, Control and Guidance
$h
[electronic resource] :
$b
Technologies by Giovanni Campolo /
$c
by Leonardo Mazzini.
250
$a
1st ed. 2016.
264
1
$a
Cham :
$b
Springer International Publishing :
$b
Imprint: Springer,
$c
2016.
300
$a
XXI, 363 p.
$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
490
1
$a
Springer Aerospace Technology,
$x
1869-1730
505
0
$a
Introduction -- The Kinematic of the flexible satellite -- The Satellite Attitude Control System -- The Dynamic of the flexible body -- The Dynamic in the Gravitational Field -- The Optimal Control Theory -- Attitude Control Methods -- Orbital Dynamic and Control -- Spacecraft Propulsion -- Sensors and Actuators technologies -- Complements to Body Kinematic -- Elements of Estimation Theory -- Basics of Lagrangian Equations -- The J2 perturbation solution -- Complements to Optimal Orbital Transfer -- Elements of Plasma physics.
520
$a
This book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators.
650
0
$a
Aerospace engineering.
$3
686400
650
0
$a
Astronautics.
$3
646219
650
0
$a
Control engineering.
$3
1249728
650
0
$a
Space sciences.
$3
715034
650
1 4
$a
Aerospace Technology and Astronautics.
$3
683885
650
2 4
$a
Control and Systems Theory.
$3
1211358
650
2 4
$a
Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics).
$3
1114976
710
2
$a
SpringerLink (Online service)
$3
593884
773
0
$t
Springer Nature eBook
776
0 8
$i
Printed edition:
$z
9783319255385
776
0 8
$i
Printed edition:
$z
9783319255392
776
0 8
$i
Printed edition:
$z
9783319368771
830
0
$a
Springer Aerospace Technology,
$x
1869-1730
$3
1257171
856
4 0
$u
https://doi.org/10.1007/978-3-319-25540-8
912
$a
ZDB-2-ENG
912
$a
ZDB-2-SXE
950
$a
Engineering (SpringerNature-11647)
950
$a
Engineering (R0) (SpringerNature-43712)
based on 0 review(s)
Multimedia
Reviews
Add a review
and share your thoughts with other readers
Export
pickup library
Processing
...
Change password
Login