[1] Farrell, J.L., “Attitude determination by kalman filtering,” Automatica, vol. 6, no. 3, 1970, pp. 419–430.
[2] Thomas, B., “Spacecraft Attitude Determination-A Magnetometer Approach,” Aalborg Universitetsforlag, Research output: Book/Report › (Thesis Ph.D.), 1999.
[3] Fisher, J. and Vadali, S. R., “Gyroless Attitude Control of Multibody Satellites Using an Unscented Kalman Filter,” J. Guid. Control. Dyn., vol. 31, no. 1, pp. 245–251, 2008.
[4] Soken, H. E. and Hajiyev, C., “In flight magnetometer calibration via unscented Kalman filter,” RAST 2011 - Proc. 5th Int. Conf. Recent Adv. Sp. Technol., 2011, pp. 885–890.
[5] Kiani M. and Pourtakdoust, S.H., “Adaptive Square-Root Cubature – Quadrature Kalman Particle Filter for satellite attitude determination using vector observations,” Acta Astronaut., vol. 105, no. 1, 2014, pp. 109–116.
[6] Sadeghi, A. R., Sabahi, M. F. and Saberali, S.M., “Using the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts,” J. Sp. Sci. Technol., vol. 9, no. 1, 2016, pp. 37–46 (In Persian).
[7] Adami, A.H. and Nosratollahi, M., “Introducing of Attitude Determination System of a LEO Satellite with Orbital Maneuver Mission,” J. Sp. Sci. Technol., vol. 4, no. 4, 2012, pp. 1–10 (In Persian).
[8] Oshman, Y. and Carmi, A., “Attitude Estimation from Vector Observations Using a Genetic-Algorithm-Embedded Quaternion Particle Filter,” J. Guid. Control. Dyn., vol. 29, no. 4, 2006, pp. 879–891
[9] Labibian, A., Pourtakdoust, S.H., Kiani, M. A., Sheikhi, A. and Alikhani, A. “Experimental validation of a novel radiation based model for spacecraft attitude estimation,” Sensors Actuators, A Phys., vol. 250, 2016, pp. 114–122.
[10] Khaniki, H.B. and Karimian, S.M.H., “Determining the heat flux absorbed by satellite surfaces with temperature data,” J. Mech. Sci. Technol., vol. 28, no. 6, 2014, pp. 2393–2398.
[11] Khaniki, H.B. and Karimian, S.M.H., “Satellite Attitude Determination Using Absorbed Heat Fluxes,” J. Aerosp. Eng., vol. 29, no. 6, 2016, p. 04016053.
[12] Labibian, A., Alikhani, A. and Pourtakdoust, S.H., “Performance of a novel heat based model for spacecraft attitude estimation,” Aerosp. Sci. Technol., vol. 70, 2017, pp. 317–327.
[13] Markley, F.L. and Crassidis, J.L., Fundamentals of Spacecraft Attitude Determination and Control, Springer, 2014.
[14] Wie, B., Space Vehicle Dynamics and Control, Second., vol. 134, no. 4. 2007.
[15] Incropera, F.P., Fundamentals of Heat and Mass Transfer, 6th Edition, John Wiley & Sons, 2005.
[16] Fortescue, P., Swinerd, G. and Stark, J., Systems Engineering Spacecraft Systems. 2011.
[17] Mittelmark, M., Sagy, S., Eriksson, M., Bauer, G., Pelikan, J. and Lindström, B., The International Handbook of Salutogenesis. 2016.
[18] “Thermal Desktop,” C&R Technol., vol. Ver. 4.8, 2005.
[19] “SINDA,” C&R Technol., vol. Ver. 4.8, 2005.
[20] Avinash, S. “How many faces of a cube you can see at a time?,” 2016.
)