Magnetic attitude control of spacecraft with flexible appendages

Proceedings of the IEEE Conference on Decision and Control

Volumn , Issue , 2006, Pages 1545-1550

  Schiavo, Francesco ^a   Lovera, Marco ^b   Astolfi, Alessandro ^c  

^a POLITECNICO DI MILANO   (Italy)

^b IMPERIAL COLLEGE LONDON   (United Kingdom)

^c UNIVERSITY OF ROME TOR VERGATA   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ATTITUDE CONTROL; COMPUTER SIMULATION; MATHEMATICAL MODELS; PROBLEM SOLVING;

FLEXIBLE APPENDAGES; MAGNETIC ACTUATORS; PRACTICAL APPLICABILITY;

SPACECRAFT;

EID: 39649113575     PISSN: 07431546     EISSN: 25762370     Source Type: Conference Proceeding    
DOI: 10.1109/cdc.2006.377766     Document Type: Conference Paper

References (18)

1. R. Wisniewski and L. Markley, "Optimal magnetic attitude control," in 14th IFAC World Congress, Beijing, China, 1999.
2. M. Lovera, E. D. Marchi, and S. Bittanti, "Periodic attitude control techniques for small satellites with magnetic actuators," IEEE Transactions on Control Systems Technology, vol. 10, no. 1, pp. 90-95, 2002.
3. M. Psiaki, "Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation," Journal of Guidance, Control and Dynamics, vol. 24, no. 2, pp. 386-394, 2001.
4. E. Silani and M. Lovera, "Magnetic spacecraft attitude control: A survey and some new results," Control Engineering Practice, Special Section on Aerospace Control, vol. 13, no. 3, pp. 357-371, 2005.
5. R. Wisniewski and M. Blanke, "Fully magnetic attitude control for spacecraft subject to gravity gradient," Automatica, vol. 35, no. 7, pp. 1201-1214, 1999.
6. C. J. Damaren, "Comments on "Fully magnetic attitude control for spacecraft subject to gravity gradient"," Automatica, vol. 38, no. 12, p. 2189, 2002.
7. C. Arduini and P. Baiocco, "Active magnetic damping attitude control for gravity gradient stabilised spacecraft," Journal of Guidance and Control, vol. 20, no. 1, pp. 117-122, 1997.
8. P. Wang and Y. Shtessel, "Satellite attitude control using only magnetic torquers," in AIAA Guidance, Navigation, and Control Conference and Exhibit, Boston, USA, 1998, 1998.
9. M. Lovera and A. Astolfi, "Spacecraft attitude control using magnetic actuators," Automatica, vol. 40, no. 8, pp. 1405-1414, 2004.
10. _, "Global magnetic attitude control of inertially pointing spacecraft," Journal of Guidance, Control and Dynamics, vol. 28, no. 5, pp. 1065-1072, 2005.
11. F. Schiavo, L. Viganó, and G. Ferretti, "Modular modelling of flexible beams for multibody systems," Multibody Systems Dynamics, 2006.
12. S. Di Gennaro, "Output attitude tracking for flexible spacecraft," Automatica, vol. 38, no. 10, pp. 1719-1726, 2002.
13. S. Joshi, A. Kelkar, and P. Maghami, "A class of stabilising controllers for flexible multibody systems," NASA, Technical paper 3494, 1995.
14. J. Wertz, Spacecraft attitude determination and control. D. Reidel Publishing Company, 1978.
15. H. Khalil, Nonlinear systems. Macmillan, 2001.
16. S. Mattsson, H. Elmqvist, and M. Otter, "Physical system modeling with Modelica," Control Engineering Practice, vol. 6, no. 4, pp. 501-510, 1998.
17. M. Lovera, "Control-oriented modelling of spacecraft attitude and orbit dynamics," Mathematical and Computer Modelling of Dynamical Systems, vol. 12, no. 1, pp. 73-88, 2006.
18. Dynasim AB, Dymola-Dynamic Modelling Laboratory, Lund, Sweden, http://www.dynasim.se/dymola.htm.