Design of spacecraft formation orbits relative to a stabilized trajectory

Journal of Guidance, Control, and Dynamics

Volumn 28, Issue 4, 2005, Pages 782-794

  Hsiao, F Y ^a,b   Scheeres, D J ^a,c  

^a UNIVERSITY OF MICHIGAN   (United States)

^b TAMKANG UNIVERSITY   (Taiwan)

^c Department of Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EIGENVALUES AND EIGENFUNCTIONS; EQUATIONS OF MOTION; FEEDBACK CONTROL; LYAPUNOV METHODS; MATHEMATICAL MODELS; MATHEMATICAL TRANSFORMATIONS; ORBITS; POSITION CONTROL; TRAJECTORIES; VELOCITY CONTROL;

LINEARIZED DYNAMICS; SPACECRAFT MOTION; STABILIZED TRAJECTORY; VELOCITY VECTOR;

SPACECRAFT;

EID: 22944464134     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.8433     Document Type: Article

References (13)

1. Barden, B. T., and Howell, K. C., "Fundamental Motions near Collinear Libration Points and Their Transitions," Journal of the Astronomical Sciences, Vol. 46, No. 4, 1998, pp. 361-378.
2. Scheeres, D. J., Hsiao, F. Y., and Vinh, N. X., "Stabilizing Motion Relative to an Unstable Orbit: Applications to Spacecraft Formation Flight," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 1, 2003, pp. 62-73.
3. Sabol, C., Burns, R., and Mclaughlin, C. A., "Satellite Formation Flying Design and Evolution," Journal of Spacecraft and Rockets, Vol. 38, No. 2, 2001, pp. 270-278.
4. Schaub, H., and Alfriend, K. T., "Impulsive Feedback Control to Establish Specific Mean Orbit Elements of Spacecraft Formations," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 4, 2001, pp. 739-745.
5. Hsiao, F. Y., and Scheeres, D. J., "The Dynamics of Formation Flight About a Stable Trajectory," Journal of the Astronautical Sciences, Vol. 50, No. 3, 2002, pp. 269-287.
6. Hussein, I., Scheeres, D. J., and Hyland, D. C., "Interferometric Observatories in Earth Orbit," Journal of Guidance, Control, and Dynamics, Vol. 27, No. 2, 2004, pp. 297-301.
7. Hsiao, F. Y., "Stabilizing and Specifying Motion Relative to Unstable Trajectories: Application to Spacecraft Formation Flight," Ph.D. Dissertation, Dept. of Aerospace Engineering, Univ. of Michigan, Ann Arbor, MI, June 2004, pp. 28-30, 64-70.
8. Marchal, C., The Three-Body Problem, Elsevier, New York, 1990, p. 64.
9. Howell, K. C., Barden, B. T., and Lo, M. W., "Application of Dynamical Systems Theory to Trajectory Design for a Libration Point Mission," Journal of the Astronautical Sciences, Vol. 45, No. 2, 1997, pp. 161-178.
10. Nemytskii, V. V., and Stepanov, V. V., Qualitative Theory of Differential Equations, Dover, New York, 1989, p. 152.
11. Bay, J. S., Fundamentals of Linear State Space Systems, McGraw-Hill, New York, 1999, p. 419.
12. Liu, G. P., and Patton, R. J., Eigenstructure Assignment for Control System Design, Chichester, New York, 1998, p. 20.
13. Subrahmanyan, P., and Tramper, D., "Eigenvector Assignment," Proceedings of the 1999 American Control Conference, Vol. 4, Pt. 4, American Automatic Control Council, New York, 1999, pp. 2238-2243.