Spacecraft Dynamics and Control

A Practical Engineering Approach

AvMarcel J. Sidi,Michael J. Rycroft

Häftad, Engelska, 2000

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Beskrivning

Satellites are used increasingly in telecommunications, scientific research, surveillance, and meteorology, and these satellites rely heavily on the effectiveness of complex onboard control systems. This 1997 book explains the basic theory of spacecraft dynamics and control and the practical aspects of controlling a satellite. The emphasis throughout is on analyzing and solving real-world engineering problems. For example, the author discusses orbital and rotational dynamics of spacecraft under a variety of environmental conditions, along with the realistic constraints imposed by available hardware. Among the topics covered are orbital dynamics, attitude dynamics, gravity gradient stabilization, single and dual spin stabilization, attitude maneuvers, attitude stabilization, and structural dynamics and liquid sloshing.

Produktinformation

Utgivningsdatum:2000-07-03
Mått:179 x 255 x 26 mm
Vikt:770 g
Format:Häftad
Språk:Engelska
Serie:Cambridge Aerospace Series
Antal sidor:432
Förlag:Cambridge University Press
ISBN:9780521787802

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Recensioner i media

"This reviewer strongly recommends this back-to-basics book on spacecraft dynamics and control to the engineering libraries and to those entering aerospace engineering schools and aerospace engineering practice. Again, the author successfully achieved his stated goal of bringing practical engineering reality into early aerospace education and it makes his book, Spacecraft Dynamics and Control well worth reading and keeping as a unique reference." Applied Mechanics Reviews

Innehållsförteckning

1. Introduction; 2. Orbital dynamics; 3. Orbital maneuvers; 4. Attitude dynamics and kinematics; 5. Gravity gradient stabilization; 6. Single and dual spin stabilization; 7. Attitude maneuvers in space; 8. Momentum-biased attitude stabilization; 9. Reaction jet attitude; 10. Structural dynamics and liquid sloshing; Appendix A. Attitude transformation in space; Appendix B. Attitude determination hardware; Appendix C. Orbit and attitude control hardware.