Open Access
Int. J. Metrol. Qual. Eng.
Volume 7, Number 1, 2016
Article Number 104
Number of page(s) 7
Published online 12 April 2016
  1. J.R. Wertz, Spacecraft attitude determination and control (Kluwer Academic Publishers, Dordrecht, Holland, 1988)
  2. R. Alonso, M.D. Shuster, Two steps: A fast robust algorithm for attitude- independent magnetometer-bias determination, J. Astronautical Sci. 50, 433–451 (2002)
  3. R. Alonso, M.D. Shuster, Attitude-independent magnetometer-bias determination: A survey, J. Astronautical Sci. 50, 453–475 (2002)
  4. M.D. Shuster, R. Alonso, Magnetometer calibration for the first Argentine spacecraft, Adv. Astronautical Sci. 91, 29–46 (1996)
  5. R. Alonso, M.D. Shuster, Centering and observability in attitude-independent magnetometer-bias determination, J. Astronautical Sci. 51, 133–141 (2003)
  6. R. Alonso, M.D. Shuster, Complete linear attitude-independent magnetometer calibration, J. Astronautical Sci. 50, 477–490 (2002)
  7. E. Kim, H. Bang, Bias estimation of magnetometer using genetic algorithm, in Proc. Int. Conf. Control Automation and System 2007, Seoul, Korea, 2007, pp. 195–198
  8. J.L. Crassidis, K. Lai, R.R. Harman, Real-time attitude-independent three-axis magnetometer calibration, J. Guidance Control Dynamics 28, 115–120 (2005) [CrossRef]
  9. L. Huang, W. Jing, Attitude-independent geomagnetic navigation using onboard complete three-axis magnetometer calibration, in Proc. 2008 IEEE Aerospace Conference, Montana, USA, 2008, pp. 1–7
  10. W. H. Steyn, A Multi-mode Attitude Detarmination and Control System for Small Satellites, Ph.D. dissertation, University of Stellenbosch, South Africa, 1995
  11. R. DaForno et al., Autonomous navigation of megSat 1: Attitude, sensor bias and scale factor estimation by EKF and magnetometer-only measurement, in Proc. 22nd AIAA International Communications Satellite Systems Conference and Exhibit, California, USA, 2004
  12. G.F. Ma, X.Y. Jiang, Unscented Kalman filter for spacecraft attitude estimation and calibration using magnetometer measurements, in Proc. 4th International Conference on Machine Learning and Cybernetics, Guangzhou, China, 2005, pp. 506–511
  13. C. Hajiyev, Orbital Calibration of microsatellite magnetometers using a linear Kalman filter, Measurement Techniques 58, 1037–1043. DOI: 10.1007/s11018-015-0838-4 [CrossRef]
  14. P. Sekhavat, Q. Gong, I.M. Ross, NPSAT I parameter estimation using unscented Kalman filter, in Proceedings of 2007 American Control Conference (IEEE, New York, USA, 2007), pp. 4445–4451
  15. T. Inamori, N. Sako, Sh. Nakasuka, Strategy of magnetometer calibration for nano-satellite missions and in-orbit performance. AIAA Guidance, Navigation, and Control Conference, 2–5 August 2010, Toronto, Ontario Canada, pp. 1–13
  16. R.E. Kalman, A new approach to linear filtering and prediciton problems, ASME J. Basic Eng. 35–45 (1960)
  17. C. Hajiyev, F. Caliskan, Fault diagnosis and reconfiguration in flight control systems (Kluwer Academic Publishers, Boston, USA, 2003)
  18. R.K. Mehra, J. Peschon, An innovations approach to fault detection and diagnosis in dynamic systems, Automatica 7, 637–640 (1971) [CrossRef]

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