New approach to mission design based on the fundamental equations of motion

Journal of Aerospace Engineering

Volumn 19, Issue 2, 2006, Pages 59-67

  Lam, Try ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

Constraints; Control methods; Dynamics; Motion; Orbits; Space exploration

Indexed keywords

CONSTRAINTS; CONTROL METHODS; MOTION; SPACE EXPLORATION;

CONSTRAINT THEORY; DYNAMICS; EQUATIONS OF MOTION; GRAVITATION; ORBITS; SPACECRAFT;

SPACE RESEARCH;

EID: 33645141531     PISSN: 08931321     EISSN: None     Source Type: Journal    
DOI: 10.1061/(ASCE)0893-1321(2006)19:2(59)     Document Type: Article

References (20)

1. Alfriend, K. T., and Schaub, H. (2000). "Dynamics and control of space-craft formations: Challenges and some solutions." J. Astronaut. Sci., 48(2), 249-267.
2. Goldreich, P. (1965). "Inclination of satellite orbits about an oblate processing planet." Astron. J., 70(1), 5-9.
3. Hussein, I. I., and Scheeres, D. J. (2004). "Effects of orbit perturbations on a class of earth-orbiting interferometric observatories." Proc., Spaceflight Mechanics Meeting, Maui, Hawaii, AAS Paper 2004-210.
4. Ilgen, M. R. (1993). "Low thrust OTV guidance using Lyapunov optimal feedback control techniques." Adv. Astronaut. Sci., 85(2), 1527-1545.
5. Kozai, Y. (1959). "The motion of close earth satellite." Astron. J., 64(1274), 367-377.
6. Kozai, Y. (1961). "Note on the motion of a close earth satellite with a small eccentricity." Astron. J., 66(3), 132.
7. Kozai, Y. (1965). "Effects of the tidal deformation of the earth on the motion of close earth satellites." Astrono. Soc. Japan, 17(4), 395-402.
8. Naasz, B. J., and Hall, C. D. (2005). "Classical element feedback control for spacecraft orbital maneuvers." J. Guid. Control Dyn., in press.
9. Pars, L. A. (1965). A treatise on analytical dynamics, Ox Bow.
10. Schaub, H., Vadali, S. R., Junkins, J. L., and Alfriend, K. T. (1999). "Spacecraft formation flying control using mean orbit elements." Proc., AAS/AIAA Astrodynamics Conf., Anchorage, Alaska, Paper No. AAS 99-310.
11. Scheeres, D. J. (1999). "The effect of C22 on orbital energy and angular momentum." Celest. Mech. Dyn. Astron., 73, 339-348.
12. Scheeres, D. J., and Guman, M. D. (2000). "Stability analysis of the Europa orbiter." Proc., AIAA/AAS Spaceflight Mechanics Meeting, Clearwater, Fla., AAS Paper 2000-154.
13. Spier, G. W. (1971). "Design and implementation of models for the double precision trajectory program (DPTRAJ)." Technical Memorandum 33-451, Jet Propulsion Laboratory.
14. Udwadia, F. E. (2002). "Constrained dynamics and tracking control of structural and mechanical systems." Proc., Conf. Dynamics and Control of Systems and Structure in Space, Cambridge University Press, Cambridge, U.K.
15. Udwadia, F. E. (2003). "A new perspective on the tracking control of nonlinear structure and mechanical systems." Proc., Royal Society of London, 459, 1783-1800.
16. Udwadia, F. E., and Kalaba, R. E. (1992). "A new perspective on constrained motion." Proc., Royal Society of London, 439, 407-410.
17. Udwadia, F. E., and Kalaba, R. E. (1996a). Analytical dynamics: A new approach, Cambridge University Press, Cambridge, U.K.
18. Udwadia, F. E., and Kalaba, R. E. (1996b). "Equations of motion for mechanical systems." J. Aerosp. Eng., 9(3), 64-69.
19. Vladimir, A. C. (1996). Orbital mechanics, 2nd Ed., American Institute of Aeronautics and Astronautics, Inc.
20. Wertz, J. R., and Larson, W. J. (1999). Space mission analysis and design, 3rd Ed., Microcosm Press and Kluwer Academic, Dordrecht, The Netherlands.