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2013 | OriginalPaper | Chapter

The Descriptions of Flight Vehicle

Authors : Yuanqing Xia, Mengyin Fu

Published in: Compound Control Methodology for Flight Vehicles

Publisher: Springer Berlin Heidelberg

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Flight vehicle attitude control system is mainly constituted by the controller, sensors, actuators, and space vehicles. Attitude sensors are responsible for attitude information and angular velocity which are calculated through the attitude determination algorithm for solving the real attitude, and then generates control signals, resulting in control of torque acting on the flight vehicle to achieve the desired state. The structure of flight vehicle block diagram is shown in Fig.4.1.

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Metadata
Title
The Descriptions of Flight Vehicle
Authors
Yuanqing Xia
Mengyin Fu
Copyright Year
2013
Publisher
Springer Berlin Heidelberg
Book
Compound Control Methodology for Flight Vehicles

Print ISBN: 978-3-642-36840-0

Electronic ISBN: 978-3-642-36841-7

Copyright Year: 2013

DOI
https://doi.org/10.1007/978-3-642-36841-7_4