Feedback control for spacecraft rendezvous and docking

Journal of Guidance, Control, and Dynamics

Volumn 22, Issue 4, 1999, Pages 609-611

  Kluever, Craig A ^a  

^a UNIVERSITY OF MISSOURI   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY VALUE PROBLEMS; CONSTRAINT THEORY; EQUATIONS OF MOTION; LYAPUNOV METHODS; MANEUVERABILITY; PROBLEM SOLVING; SPACE RENDEZVOUS; SPACECRAFT;

CONTROL LAW; OPEN LOOP CONTROL PROGRAM;

FEEDBACK CONTROL;

EID: 0032679956     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7636     Document Type: Article

References (7)

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2. Euler, E. A., "Optimal Low-Thrust Rendezvous Control," AIAA Journal, Vol. 7, No. 6, 1969, pp. 1140-1144.
3. Carter, T. E., "Optimal Power-Limited Rendezvous for Linearized Equations of Motion," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 5, 1994, pp. 1082-1086.
4. Guelman, M., and Aleshin, M., "Optimal Bounded Low Thrust Rendezvous with Fixed Terminal Approach Direction," AIAA Paper 97-648, Aug. 1997.
5. Tapley, B. D., and Fowler, W. T., "Terminal Guidance for Continuous Powered Space Vehicles," AIAA Journal, Vol. 4, No. 9, 1966, pp. 1683, 1684.
6. Yu, S., "Terminal Spacecraft Coplanar Rendezvous Control," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 4, 1995, pp. 838-842.
7. Lopez, I., and McInnes, C. R., "Autonomous Rendezvous Using Artificial Potential Function Guidance," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 2, 1995, pp. 237-241.