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Attitude determination of cubesat during eclipse considering the satellite dynamics and torque disturbance
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 Title & Authors
Attitude determination of cubesat during eclipse considering the satellite dynamics and torque disturbance
Choi, Sung Hyuk; Kang, Chul Woo; Park, Chan Gook;
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 Abstract
Attitude determination of satellite is categorized by deterministic and recursive method. The recursive algorithm using Kalman filter is widely used. Cubesat has limitation for payload to minimize then only two attitude sensors are installed which are sun sensor and magnetometer. Sun sensor measurements are useless during eclipse, however cubesat keeps estimating attitude to complete the successful mission. In this paper, Attitude determination algorithm based on Kalman filter is developed by additional term which considering the dynamics for SNUSAT-1 with disturbance torque. Verification of attitude accuracy of the algorithm is conducted during eclipse. Attitude determination algorithm is simulated to compare the performance between typical method and proposed algorithm. In addition, Attitude errors are analysed with various magnitude of disturbance torque caused by space environment.
 Keywords
Satellite Dynamics;Cubesat;Extended Kalman Filter;Space Environment;Disturbance Torque;Eclipse;
 Language
Korean
 Cited by
 References
1.
Wahba, G., "A least squares estimate of satellite attitude," SIAM review, vol. 7, no. 3, 1965, pp.409.

2.
Shuster, M. D., and Oh, S. D., "Three-axis attitude determination from vector observations," Journal of Guidance, Control, and Dynamics, vol. 4, no. 1, 1981, pp.70-77. crossref(new window)

3.
Bar-Itzhack, I. Y., and Oshman, Y., "Attitude determination from vector observations: quaternion estimation," Aerospace and Electronic Systems, IEEE Transactions on, no. 1, 1985, pp.128-136 crossref(new window)

4.
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, 1982, pp.417-429. crossref(new window)

5.
Crassidis, J. L., Markley, F. L., & Cheng, Y., "Survey of Nonlinear Attitude Estimation Methods," Journal of Guidance, Control, and Dynamics, vol. 30, no. 1, 2007, pp.12-28 crossref(new window)

6.
Kang, C. W., Park, J. H., Jeung, I. S., and Park, C. G., "Development of a robust attitude determination system for a nano-satellite." Control, Automation and Systems (ICCAS), 2014 14th International Conference on. IEEE, 2014.

7.
Cordova-Alarcon, J. R., Mendoza-Barcenas, M. A., and Solis-Santome, A., Attitude Determination System Based on Vector Observations for Satellites Experiencing Sun-Eclipse Phases, Multibody Mechatronic Systems. Springer International Publishing, 2015, pp.75-85.

8.
Mimasu, Y., van der Ha, J. C., and Narumi, T., "Attitude Determination by Magnetometer and Gyros during Eclipse," AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Honolulu, Hawaii, USA, 2008.

9.
Titterton, D., and Weston, J. L., Strapdown inertial navigation technology. Vol. 17. IET, 2004, pp.309-334.

10.
Wertz, J. R., Spacecraft Attitude Determination and Control, Kluwer Academic Publishers, Dordrecht, Netherlands, 1978, pp.113-152.

11.
Hughes, P. C., Spacecraft attitude dynamics, Courier Corporation, 2012, pp.232-280.

12.
Inamori, T., Sako, N., and Nakasuka, S., "Compensation of time-variable magnetic moments for a precise attitude control in nano-and micro-satellite missions," Advances in Space Research, vol.48, no.3, 2011, pp.432-440. crossref(new window)