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Cited by 312Spacecraft Dynamics and ControlSpacecraft Design and TechnologySpace Satellite Systems and Control

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Magnetic spacecraft attitude control: a survey and some new results

Silani, Enrico, Lovera, Marco·2005·Control Engineering Practice
DOI 10.1016/j.conengprac.2003.12.017
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Research works printed but not linked: 37

  1. Arcara, 2000, Active control of vibrations in helicopters by periodic optimal control, IEEE Transactions on Control Systems Technology, 8, 883, 10.1109/87.880590 · DOI
  2. Arduini, 1997, Active magnetic damping attitude control for gravity gradient stabilized spacecraft, Journal of Guidance and Control, 20, 117, 10.2514/2.4003 · DOI
  3. Astolfi, A., & Lovera, M. (2002). Global spacecraft attitude control using magnetic actuators. In 2002 American Control Conference, Anchorage, Alaska, USA. · DOI
  4. Bhat, S., & Dham, A. (2003). Controllability of spacecraft attitude under magnetic actuation. In IEEE conference on decision and control, Maui, Hawaii, USA. · DOI · Paper page
  5. Bittanti, S., & Colaneri, P. (1999). Periodic control. In J. Webster (Ed.), Wiley encyclopedia of electrical and electronic engineering. NewYork: Wiley. · DOI
  6. Bushenkov, 2002, Attitude stabilization of a satellite by magnetic coils, Acta Astronautica, 50, 721, 10.1016/S0094-5765(02)00011-5 · DOI
  7. Camillo, 1980, Orbit-averaged behavior of magnetic control laws for momentum unloading, Journal of Guidance, Control and Dynamics, 3, 563, 10.2514/3.19725 · DOI
  8. Clarke, 1991, Constrained receding-horizon predictive control, IEE Proceedings, 138, 347, 10.1049/ip-d.1991.0047 · DOI
  9. Colaneri, 2000, Continuous-time periodic systems in H2 and H∞, part I, Kybernetica, 36, 211
  10. Colaneri, 2000, Continuous-time periodic systems in H2 and H∞, part II, Kybernetica, 36, 329
  11. Curti, F., & Diani, F. (1999). Study on active magnetic attitude control for the Italian spacecraft bus MITA. In Proceedings of the 14th international conference on spaceflight dynamics, Iguassu Falls, Brasil.
  12. De Marchi, E., Rocco, L. D., Morea, G., & Lovera, M. (1999). Optimal magnetic momentum control for inertially pointing spacecraft. In Proceedings of the 4th ESA international conference on spacecraft guidance, navigation and control systems, ESTEC, Noordwijk, The Netherlands.
  13. Fritzson, P., & Bunus, 2002. Modelica—a general object-oriented language for continuous and discrete-event system modelling and simulation. In Proceedings of the 35th IEEE annual simulation symposium, San Diego, CA.
  14. Hablani, 1995, Comparative stability analysis and performance of magnetic controllers for bias momentum satellites, Journal of Guidance, Control and Dynamics, 18, 1313, 10.2514/3.21547 · DOI
  15. Kwon, 1978, On feedback stabilization of time-varying discrete linear systems, IEEE Transactions On Automatic Control, AC-23, 479, 10.1109/TAC.1978.1101749 · DOI
  16. Lagrasta, S., & Bordin, M. (1996). Normal mode magnetic control of LEO spacecraft with integral action. In AIAA guidance, navigation and control conference, San Diego, USA. · DOI
  17. Lovera, M. (2000). Periodic H∞ attitude control for satellites with magnetic actuators. In 3rd IFAC symposium on robust control design, Prague, Czech Republic. · DOI
  18. Lovera, 2001, Optimal magnetic momentum control for inertially pointing spacecraft, European Journal of Control, 7, 30, 10.1016/S0947-3580(01)70936-3 · DOI
  19. Lovera, M. (2003). Modelling and simulation of spacecraft attitude dynamics. In Proceedings of the 4th international symposium on mathematical modelling, Vienna, Austria.
  20. Lovera, M., & Astolfi, A. (2001). Global attitude regulation using magnetic control. In IEEE conference on decision and control, Tampa, FL, USA. · DOI
  21. Lovera, M., & Astolfi, A. (2003). Global magnetic attitude control of spacecraft in the presence of gravity gradient. In IEEE conference on decision and control, Maui, Hawaai, USA. · DOI
  22. Lovera, 2002, Periodic attitude control techniques for small satellites with magnetic actuators, IEEE Transactions on Control Systems Technology, 10, 90, 10.1109/87.974341 · DOI
  23. Martel, F., Pal, P., & Psiaki, M. (1988). Active magnetic control system for gravity gradient stabilized spacecraft. In 2nd annual AIAA/USU conference on small satellites, Logan (Utah), USA.
  24. Otter, M., & Olsson, H. (2002). New features in Modelica 2.0. In Proceedings of the 2nd international modelica conference, Oberpfaffenhofen, Germany.
  25. Psiaki, M. (2000). Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation. In AIAA guidance, navigation, and control conference, Denver, Colorado, USA. · DOI
  26. Psiaki, 2001, Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation, Journal of Guidance, Control and Dynamics, 24, 386, 10.2514/2.4723 · DOI
  27. Rawlings, 1993, The stability of constrained receding horizon control, IEEE Transactions on Automatic Control, 38, 1512, 10.1109/9.241565 · DOI
  28. Steyn, 1994, Fuzzy control for a non-linear MIMO plant subject to control constraints, IEEE Transactions on Systems, Man and Cybernetics, 24, 1565, 10.1109/21.310540 · DOI
  29. Stickler, 1976, An elementary magnetic attitude control system, Journal of Spacecraft and Rockets, 13, 282, 10.2514/3.57089 · DOI
  30. Varga, 1998, Gradient-based approach to solve optimal periodic output feedback control problems, Automatica, 34, 477, 10.1016/S0005-1098(97)00214-8 · DOI
  31. Wang, P., Shtessel, Y. (1999). Satellite attitude control via magnetorquers using switching control laws. In Proceedings of the 14th IFAC world congress, Beijing, China. · DOI
  32. Wen, 1991, The attitude control problem, IEEE Transactions on Automatic Control, 36, 1148, 10.1109/9.90228 · DOI
  33. Wisniewski, R. (1996). Satellite attitude control using only electromagnetic actuation. Ph.D. thesis, Aalborg University, Denmark. · DOI
  34. Wisniewski, 2000, Linear time-varying approach to satellite attitude control using only electromagnetic actuation, Journal of Guidance, Control and Dynamics, 23, 640, 10.2514/2.4609 · DOI
  35. Wisniewski, 1999, Fully magnetic attitude control for spacecraft subject to gravity gradient, Automatica, 35, 1201, 10.1016/S0005-1098(99)00021-7 · DOI
  36. Wisniewski, R., & Markley, L. (1999). Optimal magnetic attitude control. In Proceedings of the 14th IFAC world congress, Beijing, China. · DOI
  37. Wisniewski, R., & Stoustrup, J. (2002). Periodic H2 synthesis for spacecraft attitude determination and control with a vector magnetometer and magnetorquers. In Proceedings of the 1st IFAC workshop on periodic control systems, (pp. 121–126), Cernobbio-Como, Italy.

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Metadata

Authors
Silani, E., & Lovera, M.
Affiliations
Politecnico di Milano (IT)
Corresponding author
Silani, Enrico
ORCID
Lovera, Marco
Venue
Control Engineering Practice
Publisher
Elsevier BV
Published
2005-03
Volume
13
Issue
3
Pages
357-371
ISSN
0967-0661 (ISSN-L)
DOI
10.1016/j.conengprac.2003.12.017
OpenAlex
W2011561785
Cited by
312
References
2
Citations by year
2026: 5 · 2025: 9 · 2024: 13 · 2023: 8 · 2022: 15 · 2021: 10 · 2020: 22 · 2019: 23 · 2018: 9 · 2017: 24 · 2016: 26 · 2015: 22 · 2014: 17 · 2013: 19 · 2012: 20
FWCI
12.27
Type
journal article
Language
en
Open access
closed
Licence
Locations
  • Control Engineering Practice (publishedVersion)
  • Virtual Community of Pathological Anatomy (University of Castilla La Mancha) (submittedVersion)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
  • Physical Sciences › Engineering › Aerospace Engineering › Space Satellite Systems and Control
Keywords
magnetic attitude control, spacecraft attitude stabilization, small satellites, magnetic actuators, periodic control, nonlinear control, model predictive control, attitude control

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