Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering

Aerospace Science and Technology

Volumn 10, Issue 7, 2006, Pages 636-643

  Liu, Hui ^a   Li, Junfeng ^a   Hexi, Baoyin ^a  

^a TSINGHUA UNIVERSITY   (China)

Author keywords

Entire formation maneuvering; Sliding mode control; Spacecraft formation flying

Indexed keywords

EARTH-ORBITING SPACECRAFTS; ENTIRE FORMATION MANEUVERING; SPACECRAFT FORMATION FLYING (SFF); STABILITY ANALYSIS;

AEROSPACE ENGINEERING; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; FUEL CONSUMPTION; LYAPUNOV METHODS; MANEUVERABILITY; MATHEMATICAL MODELS; SLIDING MODE CONTROL; SYSTEMS ANALYSIS;

SPACECRAFT;

EID: 33749511995     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2006.04.008     Document Type: Article

References (20)

1. Alfriend K., and Schaub H. Dynamics and control of spacecraft formations: Challenges and some solutions. Journal of Astronautical Sciences 48 2 (2000) 249-267
2. Balch T., and Arkin C. Behavior-based formation control for multirobot teams. IEEE Transactions on Robotics and Automation 14 6 (1998) 926-939
3. Bread R.W., Lawton J., and Hadaegh F.Y. A coordination architecture for spacecraft formation control. IEEE Transactions on Control Systems Technology 9 6 (2001) 777-790
4. Clohessy W.H., and Wiltshire R.S. Terminal guidance system for satellite rendezvous. Journal of Aerospace Science 27 9 (1960) 653-658
5. de Queiroz M.S., Kapilar V., and Yan Q. Adaptive nonlinear control of multiple spacecraft formation flying. Journal of Guidance, Control, and Dynamics 23 3 (2000) 385-390
6. Dwyer T.A.W., and Sira-Ramirez H. Variable-structure control of spacecraft attitude maneuvers. Journal of Guidance, Control, and Dynamics 11 3 (1988) 262-270
7. F.Y. Hadaegh, W.M. Lu, P.K.C. Wang, Adaptive control of formation flying spacecraft for interferometry, in: International Federation of Automatic Control Conference on Large Scale Systems, Rio Patras, Greece, 1998, pp. 97-102
8. Iyer A.R., and Singh S.N. Variable structure slewing control and vibration damping of flexible spacecraft. Acta Astronautica 25 2 (1988) 1-9
9. Kang W., Sparks A., and Banda S. Coordinated control of multisatellite systems. Journal of Guidance, Control, and Dynamics 24 2 (2001) 360-368
10. Kapila V., Sparks A.G., Buffington J.M., and Yan Q. Spacecraft formation flying: Dynamics and control. Journal of Guidance, Control, and Dynamics 23 3 (2000) 561-564
11. D.J. Lee, P.Y. Li, Formation and maneuver control for multiple spacecraft, in: Proceedings of American Control Conference, vol. 1, 2003, pp. 278-283
12. Massey T., and Shtessel Y. Continuous traditional and high-order sliding modes for satellite formation control. Journal of Guidance, Control, and Dynamics 28 4 (2005) 826-831
13. Redding D.C., Adams N.J., and Kubiak E.T. Linear-quadratic stationkeeping for the STS orbiter. Journal of Guidance, Control, and Dynamics 12 2 (1989) 248-255
14. W. Ren, R.W. Bread, Formation feedback control for multiple spacecraft via virtual structures, in: IEE Proceedings - Control Theory and Applications, vol. 151, No. 3, 2004, pp. 357-368
15. D.P. Scharf, F.Y. Hadaegh, S.R. Ploen, A survey of spacecraft formation flying guidance and control (part II): Control, in: Proceedings of the 2004 American Control Conference, Boston, MA, June 30-July 2, 2004
16. Utkin V.I. Variable structure systems with sliding modes. IEEE Trans. Automatic Control. 22 (1977) 212-222
17. Vassar R.H., and Sherwood R.B. Formationkeeping for a pair of satellites in a circular orbit. Journal of Guidance, Control, and Dynamics 8 2 (1985) 235-242
18. Wang P.K.C., and Hadaegh F.Y. Coordination and control of multiple microspacecraft moving in formation. Journal of Astronautical Sciences 44 3 (1996) 315-355
19. Wang P.K.C., Hadaegh F.Y., and Lau K. Synchronized formation rotation and attitude control of multiple free-flying spacecraft. Journal of Guidance, Control, and Dynamics 22 1 (1999) 28-35
20. Yeh H.-H., Nelson E., and Sparks A. Nonlinear tracking control for satellite formations. Journal of Guidance, Control, and Dynamics 25 2 (2002) 376-386