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Flexible Spacecraft Dynamics, Control and Guidance : ITechnologies 2016
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eBay-Artikelnr.:397225014555
Artikelmerkmale
- Artikelzustand
- Neuwertig
- Hinweise des Verkäufers
- “text unmarked”
- Item Height
- 1.2 in
- ISBN
- 9783319255385
Über dieses Produkt
Product Identifiers
Publisher
Springer International Publishing A&G
ISBN-10
331925538X
ISBN-13
9783319255385
eBay Product ID (ePID)
8038672925
Product Key Features
Number of Pages
Xxi, 363 Pages
Language
English
Publication Name
Flexible Spacecraft Dynamics, Control and Guidance : in Cooperation with Giovanni Campolo
Publication Year
2015
Subject
Physics / Astrophysics, Electrical, Aeronautics & Astronautics
Type
Textbook
Subject Area
Technology & Engineering, Science
Series
Springer Aerospace Technology Ser.
Format
Hardcover
Dimensions
Item Weight
248.2 Oz
Item Length
9.3 in
Item Width
6.1 in
Additional Product Features
Intended Audience
Scholarly & Professional
Dewey Edition
23
Number of Volumes
1 vol.
Illustrated
Yes
Dewey Decimal
629.4742
Table Of Content
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.
Synopsis
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.
LC Classification Number
TL1-4050
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