Analytical mechanics of space systems
I tiakina i:
| Kaituhi matua: | |
|---|---|
| Kaituhi rangatōpū: | |
| Ētahi atu kaituhi: | |
| Hōputu: | Tāhiko īPukapuka |
| Reo: | Ingarihi |
| I whakaputaina: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
c2009.
|
| Putanga: | 2nd ed. |
| Rangatū: | AIAA education series.
|
| Ngā marau: | |
| Urunga tuihono: | An electronic book accessible through the World Wide Web; click to view |
| Ngā Tūtohu: |
Tāpirihia he Tūtohu
Kāore He Tūtohu, Me noho koe te mea tuatahi ki te tūtohu i tēnei pūkete!
|
Rārangi ihirangi:
- 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.