International Journal of Aeronautical and Space Sciences

  • 제9권1호
  • /
  • Pages.147-161
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  • 2008
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  • 2093-274X(pISSN)
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  • 2093-2480(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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Kalman Filtering for Spacecraft Attitude Estimation by Low-Cost Sensors

  • 발행 : 2008.05.10
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초록

In this paper, fine attitude estimation using low-cost sensors for attitude pointing missions of spacecraft is addressed. Attitude kinematics and gyro models including bias models are in general utilized to estimate spacecraft attitude and angular rate. However, a linearized model and a transition matrix are derived in this paper from nonlinear spacecraft dynamics with external disturbances. A Kalman filtering technique is applied and offers relatively high estimation accuracy under dynamic uncertainties. The proposed approach is demonstrated using numerical simulations.

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참고문헌

  1. Humphreys, T.E., 'Attitude Determination for Small Satellites with Modest Pointing Constraintsn', it Utah State University Report
  2. Psiaki, M.L., Martel, F., and Pal. P.K,, 'Three-Axis Attitude Determination via Kalman Filtering of Magnetometer Data', Journal of Guidance, Control, and Dynamics, Vol. 13, No. 3, 1989, pp. 506-514 https://doi.org/10.2514/3.25364
  3. Landiech, P., 'Extensive Use of Magnetometers and Magnetic torquers for Small Satellites Attitude Estimation and Control', AIAA Paper AAS 95-012, 1995
  4. Crassidis, J.L., and Markley, F.L., 'Predictive Filtering for Attitude Estimation Without Rate Sensors', Journal of Guidance, Control, and Dynamics, Vol. 20, No. 3, May.June 1997
  5. Lefferts, E.J., Markley, F.L., and Shuster, M.D., 'Kalman Filtering for Spacecraft Attitude Estimation', Journal of Guidance, Control, and Dynamics, Vol. 5, No.5, Sept.-Oct. 1982, pp. 417-429 https://doi.org/10.2514/3.56190
  6. Bar-Itzhack, I.Y., and Oshman, Y., 'Attitude Determination from Vector Observations: Quaternion Estimation', IEEE Trans. on Aerospace and Electronic Systems Vol. AES-21, No. 1, Jan. 1985

피인용 문헌

  1. Uncorrelated unscented filtering for spacecraft attitude determination vol.67, pp.1-2, 2010, https://doi.org/10.1016/j.actaastro.2009.12.017
  2. Theoretical Research on Full Attitude Determination Using Geomagnetic Gradient Tensor vol.68, pp.05, 2015, https://doi.org/10.1017/S0373463315000259
  3. An Attitude Filtering and Magnetometer Calibration Approach for Nanosatellites vol.19, pp.1, 2018, https://doi.org/10.1007/s42405-018-0020-8