[1] Likins, P.W., and Fleischer, G.E., "Results of Flexible Spacecraft Attitude Control Studies Utilizing Hybrid Coordinates", Journal of Spacecraft and Rockets, Vol. 8(3), pp. 264-273, (1971).
[2] Johnston, J.D., and Thornton E.A., "Thermally Induced Dynamics of Satellite Solar Panels", Journal of Spacecraft and Rockets, Vol. 37(5), pp. 604-613, (2000).
[3] Kubota, T., Hashimoto, T., Sawai, S., Kawaguchi, J.I., Ninomiya, K., Uo, M., and Baba, K., "An Autonomous Navigation and Guidance System for MUSES-C Asteroid Landing", Acta Astronautica, Vol. 52(2-6), pp. 125-131, (2003).
[4] Wie, B., and Plescia, C.T., "Attitude Stabilization of Flexible Spacecraft During Stationkeeping Maneuvers", Journal of Guidance, Control and Dynamics (JGCD), Vol. 7(4), pp. 430-436, (1984).
[5] Al-Saif, K.A., Foda, M.A., and Aldakkan, K., "Suppression of Microvibrations of Low-earth-orbit Satellites with Flexible Solar Panels", Journal of Aerospace Engineering, Vol. 25(1), pp. 117-124, (2012).
[6] He, W., and Ge, S.S., "Dynamic Modeling and Vibration Control of a Flexible Satellite", IEEE Transactions on Aerospace and Electronic Systems, Vol. 51(2), pp. 1422-1431, (2015).
[7] Rad, H.K., Salarieh, H., Alasty, A., and Vatankhah, R., "Boundary Control of Flexible Satellite Vibration in Planar Motion", Journal of Sound and Vibration, Vol. 432, pp. 549-568, (2018).
[8] Avanzini, G., de Angelis, E.L., Giulietti, F., and Serrano, N., "Attitude Control of Low Earth Orbit Satellites by Reaction Wheels and Magnetic Torquers", Acta Astronautica, Vol. 160, pp. 625-634, (2019).
[9] Murilo, A., De Deus Peixoto, P.J., De Souza, L.C.G., and Lopes, R.V., "Real-time Implementation of a Parameterized Model Predictive Control for Attitude Control Systems of Rigid-flexible Satellite", Mechanical Systems and Signal Processing, Vol. 149, pp. 107-129, (2021).
[10] Bang, H., Ha, C.K., and Kim J.H., "Flexible Spacecraft Attitude Maneuver by Application of Sliding Mode Control", Acta Astronautica, Vol. 57(11), pp. 841-850, (2005).
[11] Bai, H., Huang, C., and Zeng, J., "Robust Nonlinear H∞ Output-feedback Control for Flexible Spacecraft Attitude Manoeuvring", Transactions of the Institute of Measurement and Control, Vol. 41(7), pp. 2026-2038, (2019).
[12] Cheng, X., Yuan, L.I.U., Yi, Q.I.N., Feng,W.A.N.G., and Zhang, J., "Coordinated Attitude Control for Flexible Spacecraft Formation with Actuator Configuration Misalignment", Chinese Journal of Aeronautics, Vol. 34(3), pp. 176-186, (2020).
[13] Lee, J., Kang, D.E., and Park, C., "Geometric Robust Adaptive Control for Satellite Attitude Tracking with Reaction Wheels", Acta Astronautica, Vol. 179, pp. 238-252, (2021).
[14] Malekzadeh, M., "Robust Control of Flexible Spacecraft Considering Actuator Dynamic", Modares Mechanical Engineering, Vol. 14(15), pp. 225-230, (2015).
[15] Malekzadeh, M., "Quaternion Based Active Control of a Flexible Spacecraft", The 15th International Conference of the Iranian Aerospace Association, 5-7 November, Tehran, Iran, (2016).
[16] Sadeghian Bafghi, S., Fathi, M., Rahbar, N., "Control the Elevation Angle of the Flexible Satellite Model-based Predictive Controller Assistance Neural Network", Iranian Mechanical Engineering Journal, Vol. 18(1), pp. 22-40, (2016).
[17] Li, Y., and Ye, D., "Robust PID Controller for Flexible Satellite Attitude Control under Angular Velocity and Control Torque Constraint", Asian Journal of Control, Vol. 22(3), pp. 1327-1344, (2020).
[18] Sidi, M.J., "Spacecraft Dynamics and Control: a Practical Engineering Approach", Cambridge Aerospace Series 7, First Published, Press Syndicate of the University of Cambridge (Cambridge University Press), New York, USA, (1997).