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Bibliografická citace

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EB
ONLINE
2nd ed.
Reston, Va. : American Institute of Aeronautics and Astronautics, c2009
1 online resource (xxi, 793 p.) : ill
Externí odkaz    Plný text PDF 
   * Návod pro vzdálený přístup 


ISBN 9781600867224 (electronic bk.)
ISBN 1600867219 (alk. paper)
ISBN 9781600867217 (alk. paper)
AIAA education series
Includes bibliographical references and index
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.
Electronic reproduction. Ann Arbor, MI : ProQuest, 2015. Available via World Wide Web. Access may be limited to ProQuest affiliated libraries
001807913
full
(Au-PeEL)EBL3111684
(CaPaEBR)ebr10516789
(MiAaPQ)EBC3111684
(OCoLC)922979132

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