Peter C. Hughes

Spacecraft Attitude Dynamics (eBook, ePUB)

• Format: ePub

Produktbeschreibung

Pointing a satellite in the right direction requires an extremely complex system one that describes the satellite's orientation and at the same time predicts and either uses or neutralizes external influences.

From its roots in classical mechanics and reliance on stability theory to the evolution of practical stabilization ideas, Spacecraft Attitude Dynamics offers comprehensive coverage of environmental torques encountered in space; energy dissipation and its effects on the attitude stability of spinning bodies; motion equation for four archetypical systems derived and used repeatedly throughout the text; orientation parameters (not limited to Euler angles); illustrations of key concepts with on-orbit flight data; and typical engineering hardware, with examples of the implementation of dynamic ideas.

Suitable as a text for advanced undergraduates and graduate students, this unified treatment is also a valuable reference for professional engineers studying the analysis and application of modern spacecraft attitude dynamics. The sole prerequisites are a fundamental knowledge of vector dynamics and matrix algebra. Over 250 diagrams appear throughout the text, along with extensive problem sets at the end of each chapter, 350 references (cited, interpreted, and placed in perspective to reinforce the material), and two helpful appendixes.

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Produktdetails

• Verlag: Guilford Publications
• Seitenzahl: 592
• Erscheinungstermin: 23. Mai 2012
• Englisch
• ISBN-13: 9780486140131
• Artikelnr.: 40021839

Inhaltsangabe

1. Introduction 2. Rotational Kinematics 3. Attitude Motion Equations 4.
Attitude Dynamics of a Rigid Body 5. Effect of Internal Energy Dissipation
on the Directional Stability of Spinning Bodies 6. Directional Stability of
Multispin Vehicles 7. Effect of Internal Energy Dissipation on the
Directional Stability of Gyrostats 8. Spacecraft Torques 9. Gravitational
Stabilization 10. Spin Stabilization in Orbit 11. Dual-Stabilization in
Orbit: Gyrostats and Bias Momentum Satellites Appendixes References Index