Cited by 14Spacecraft Dynamics and ControlControl and Stability of Dynamical SystemsSpacecraft Design and Technology

The DOI matches its Crossref record; 1 of the 1 references it cites were found in a registry or an index.

Attitude Stabilization of a Nadir-Pointing Small Satellite Using Only Magnetic Actuators

Reyhanoglu, Mahmut, Ton, Chau, Drakunov, Sergey·2009·IFAC Proceedings Volumes

Overview

Integrity signals

Registry

Crossref · 10.3182/20090921-3-tr-3005.00052

Cites

1 of 1 references verified0 citation errors · 0 not checkable

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Claims other papers make about this one

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  • References [Lovera and Astolfi, 2006] - [Reyhanoglu and Drakunov, 2009] include the effect of a favorable gravity gradient disturbance torque to bring the satellite to an Earth-pointing equilibrium, guaranteeing almost global stability.

    “Finally, references [Lovera and Astolfi, 2006] - [Reyhanoglu and Drakunov, 2009] include the effect of a favorable gravity gradient disturbance torque to bring the satellite to an Earth-pointing equilibrium, guaranteeing almost global stability.”

Citations

Cites

Flagged first, then by citations

Research works printed but not linked: 26

  1. Alfriend, 1975, Magnetic attitude control system for dual-spin satellites, AIAA Journal, 13, 817, 10.2514/3.60443 · DOI
  2. Arduini, 1997, Active magnetic damping attitude control for gravity gradient stabilized spacecraft, Journal of Guidance, Control, and Dynamics, 20, 117, 10.2514/2.4003 · DOI
  3. Bhat, 2005, Controllability of nonlinear time-varying systems: applications to spacecraft attitude control using magnetic actuation, IEEE Transactions on Automatic Control, 50, 1725, 10.1109/TAC.2005.858686 · DOI
  4. Bloch, 1992, Control and stabilization of nonholonomic dynamic systems, IEEE Transactions on Automatic Control, 37, 1746, 10.1109/9.173144 · DOI
  5. Byrnes, 1991, On the attitude stabilization of rigid spacecraft, IFAC Journal Automatica, 27, 87, 10.1016/0005-1098(91)90008-P · DOI
  6. Drakunov, 1994, Sliding mode control with multiple equilibrium manifolds, Proceedings of ME94 International Congress and Exposition, 55-1, 101
  7. Goel, 1979, Magnetic attitude control of a momentum-biased satellite in near-equatorial orbit, Journal of Guidance and Control, 2, 334, 10.2514/3.55884 · DOI
  8. Krishnan, 1995, Attitude stabilization of a rigid spacecraft using two momentum wheel actuators, AIAA Journal of Guidance, Control, and Dynamics, 18, 256, 10.2514/3.21378 · DOI
  9. Krishnan, 1994, Attitude stabilization of a rigid spacecraft using two controls: a nonlinear control approach based on spacecraft dynamics, IFAC Journal Automatica, 30, 1023, 10.1016/0005-1098(94)90196-1 · DOI
  10. Lawton, J. and Beard, R.W. (2001). Model independent eigenaxis maneuvers using quaternion feedback. Proceedings of the American Control Conference, 2339- 2344. · DOI
  11. Lizarralde, 1996, Attitude control without velocity measurement: A passivity approach, IEEE Transactions on Automatic Control, 41, 468, 10.1109/9.486654 · DOI
  12. Lovera, 2004, Spacecraft attitude control using magnetic actuators, IFAC Journal Automatica, 40, 1405, 10.1016/j.automatica.2004.02.022 · DOI · Paper page
  13. Makovec, K.L. (2001). Satellite attitude control using only electromagnetic actuation. M.S. Thesis, Virginia Polytechnic Institute and State University, Virginia, USA.
  14. Morin, 1995, Time-varying feedback stabilization of the attitude of a rigid spacecraft with two controls, Systems and Control Letters, 25, 375, 10.1016/0167-6911(94)00095-D · DOI
  15. Musser, 1989, Autonomous spacecraft attitude control using magnetic torquing only, Proceedings of Flight Mechanics/Estimation Theory Symposium, 23
  16. Psiaki, 2001, Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation, AIAA Journal of Guidance, Control, and Dynamics, 24, 386, 10.2514/2.4723 · DOI
  17. Renard, 1967, Command laws for magnetic attitude control of spin-stabilized earth satellites, Journal of Spacecraft and Rockets, 4, 156, 10.2514/3.28828 · DOI
  18. Reyhanoglu, 1999, Dynamics and control of a class of underactuated mechanical systems, IEEE Transactions on Automatic Control, 44, 1663, 10.1109/9.788533 · DOI · Paper page
  19. Shigehara, 1972, Geomagnetic attitude control of an axisymmetric spinning satellite, Journal of Spacecraft and Rockets, 9, 391, 10.2514/3.61700 · DOI
  20. Sorenson, 1971, A magnetic attitude control system for an axisymmetric spinning spacecraft, Journal of Spacecraft and Rockets, 8, 441, 10.2514/3.59677 · DOI
  21. Tsiotras, 1998, Further passivity results for the attitude control problem, IEEE Transactions on Automatic Control, 43, 1597, 10.1109/9.728877 · DOI
  22. Wang, 1998, Satellite attitude control using only magnetic torquers, Proceedings of the AIAA Guidance, Navigation, and Control Conference, 1490
  23. Wen, 1991, The attitude control problem, IEEE Transactions on Automatic Control, 36, 1148, 10.1109/9.90228 · DOI
  24. Wheeler, 1967, Spinning spacecraft attitude control via the environmental magnetic field, Journal of Spacecraft and Rockets, 4, 1631, 10.2514/3.29145 · DOI
  25. Wisniewski, R. (1996). Satellite attitude control using only electromagnetic actuation. Ph.D. Thesis, Aalborg University, Denmark. · DOI
  26. Wisniewski, 1999, Fully magnetic attitude control for spacecraft subject to gravity gradient, IFAC Journal Automatica, 35, 1201, 10.1016/S0005-1098(99)00021-7 · DOI

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Metadata

Authors
Reyhanoglu, M., Ton, C., & Drakunov, S.
Affiliations
Embry-Riddle Aeronautical University Daytona Beach Florida Campus (US)
Corresponding author
  • Reyhanoglu, Mahmut
  • Ton, Chau
  • Drakunov, Sergey
Venue
IFAC Proceedings Volumes
Publisher
Elsevier BV
Published
2009
Volume
42
Issue
19
Pages
292-297
ISSN
1474-6670 (ISSN-L)
OpenAlex
W1996458447
Cited by
14
References
1
Citations by year
2025: 2 · 2022: 3 · 2019: 3 · 2017: 1 · 2016: 1 · 2014: 1 · 2012: 2
FWCI
1.96
Type
conference paper
Language
en
Open access
closed
Locations
  • IFAC Proceedings Volumes (publishedVersion)
  • Scholarly Commons (Embry–Riddle Aeronautical University) (submittedVersion)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
  • Physical Sciences › Engineering › Control and Systems Engineering › Control and Stability of Dynamical Systems
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
Keywords
small satellites, magnetic attitude control, nadir pointing, attitude stabilization, passivity-based control, low Earth orbit, three-axis attitude control, angular velocity measurement

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