Analytical mechanics of space systems / Hanspeter Schaub, John L. Junkins [E-Book]
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Full text |
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Personal Name(s): | Schaub, Hanspeter. |
Junkins, John L. | |
Edition: |
2nd edition |
Imprint: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
c2009
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Physical Description: |
xxi, 793 pages : illustrations |
Note: |
englisch |
Series Title: |
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"name" and "number" keys or a flat string containing only the series
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AIAA education series
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Subject (LOC): |
LEADER | 02150nam a2200337 a 4500 | ||
---|---|---|---|
001 | EBC3111684 | ||
003 | MiAaPQ | ||
008 | 090821s2009 vaua sb 001 0 eng d | ||
035 | |a (Sirsi) a736718 | ||
041 | |a eng | ||
082 | 0 | 4 | |a 521 |2 22 |
100 | 1 | |a Schaub, Hanspeter. | |
245 | 1 | 0 | |a Analytical mechanics of space systems / |c Hanspeter Schaub, John L. Junkins |h [E-Book] |
250 | |a 2nd edition | ||
264 | 1 | |a Reston, Va. : |b American Institute of Aeronautics and Astronautics, |c c2009 |e (ProQuest) | |
300 | |a xxi, 793 pages : |b illustrations | ||
336 | |a text |b txt |2 rdacontent | ||
337 | |a computer |b c |2 rdamedia | ||
338 | |a online resource |b cr |2 rdacarrier | ||
490 | |a AIAA education series | ||
500 | |a englisch | ||
505 | 0 | |a Particle kinematics -- Newtonian mechanics -- Rigid body kinematics -- Eulerian mechanics -- Generalized methods of analytical dynamics -- Variational methods in analytical dynamics -- Hamilton's generalized formulations of analytical dynamics -- Nonlinear spacecraft stability and control -- Classical two-body problem -- Restricted three-body problem -- Gravitational potential field models -- Perturbation methods -- Transfer orbits -- Spacecraft formation flying -- Appendix A. Transport theorem derivation using linear algebra -- Appendix B. Various Euler angle transformations -- Appendix C. MRP identity proof -- Appendix D. Conic section transformations -- Appendix E. Numerical subroutines library -- Appendix F. First-order mapping between mean and osculating orbit elements -- Appendix G. Direct linear mapping between Cartesian Hill frame coordinates and orbit element differences -- Appendix H. Hamel coefficients for the rotational motion of a rigid body. | |
650 | 0 | |a Celestial mechanics. | |
650 | 0 | |a Differentiable dynamical systems. | |
650 | 0 | |a Orbital mechanics. | |
650 | 0 | |a Space vehicles |x Control systems. | |
700 | 1 | |a Junkins, John L. | |
856 | 4 | 0 | |u https://ebookcentral.proquest.com/lib/fz/detail.action?docID=3111684 |z Volltext |
915 | |a zzwFZJProQuest | ||
596 | |a 1 | ||
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