Flexible Spacecraft Dynamics, Control and Guidance Technologies by Giovanni Campolo /

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 th...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής
Κύριος συγγραφέας: Mazzini, Leonardo (Συγγραφέας)
Συγγραφή απο Οργανισμό/Αρχή: SpringerLink (Online service)
Μορφή: Ηλεκτρονική πηγή Ηλ. βιβλίο
Γλώσσα:English
Έκδοση: Cham : Springer International Publishing : Imprint: Springer, 2016.
Σειρά:Springer Aerospace Technology,
Θέματα:
Διαθέσιμο Online:Full Text via HEAL-Link
LEADER 03294nam a22004935i 4500
001 978-3-319-25540-8
003 DE-He213
005 20170520141637.0
007 cr nn 008mamaa
008 151027s2016 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 
040 |d GrThAP 
050 4 |a TL787-4050.22 
072 7 |a TRP  |2 bicssc 
072 7 |a TTDS  |2 bicssc 
072 7 |a TEC002000  |2 bisacsh 
082 0 4 |a 629.1  |2 23 
100 1 |a Mazzini, Leonardo.  |e author. 
245 1 0 |a Flexible Spacecraft Dynamics, Control and Guidance  |h [electronic resource] :  |b Technologies by Giovanni Campolo /  |c by Leonardo Mazzini. 
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 Engineering. 
650 0 |a Aerospace engineering. 
650 0 |a Astronautics. 
650 0 |a Control engineering. 
650 1 4 |a Engineering. 
650 2 4 |a Aerospace Technology and Astronautics. 
650 2 4 |a Control. 
650 2 4 |a Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics). 
710 2 |a SpringerLink (Online service) 
773 0 |t Springer eBooks 
776 0 8 |i Printed edition:  |z 9783319255385 
830 0 |a Springer Aerospace Technology,  |x 1869-1730 
856 4 0 |u http://dx.doi.org/10.1007/978-3-319-25540-8  |z Full Text via HEAL-Link 
912 |a ZDB-2-ENG 
950 |a Engineering (Springer-11647)