[1] L. Mazzini, Springer Aerospace Technology Flexible Spacecraft Dynamics, Control and Guidance. Cham: Springer International Publishing, 2016.
[2] M. Zarourati, M. Mirshams, and M. Tayefi, “Robust Hybrid Attitude Tracking and Vibration Suppression Control of a Remote Sensing Flexible Satellite Based on Command Shaping Method,” Arab. J. Sci. Eng., pp. 1–9, Oct. 2025.
[3] P. Gasbarri, R. Monti, and M. Sabatini, “Very large space structures: Non-linear control and robustness to structural uncertainties,” Acta Astronaut., vol. 93, pp. 252–265, Jan. 2014.
[4] M. Zarourati, M. Mirshams, and M. Tayefi, “Adaptive Robust Attitude Control and Vibration Suppression of a Flexible Satellite in Imaging Maneuver,” J. Sp. Sci. Technol., vol. 18, no. 1, pp. 78–91, 2025.
[5] M. Zarourati, M. Mirshams, and M. Tayefi, “A Review on Underactuated Attitude Control of Reaction Wheel Actuated Satellites,” J. Sp. Sci. Technol., vol. 18, no. 2, pp. 83–119, 2025.
[6] J. Wang and D.-X. Li, Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters. Singapore: Springer Singapore, 2022.
[7] C. Chiappa, G. Bodineau, S. Boulade, and C. Beugnon, “(μ -Mu) -iteration technique: Application to attitude control of satellite with large flexible appendages,” Proc. 44th IEEE Conf. Decis. Control. Eur. Control Conf. CDC-ECC ’05, vol. 2005, pp. 641–646, 2005.
[8] M. Zarourati, M. Mirshams, and M. Tayefi, “Integrated vibration suppression-based attitude tracking control of a flexible satellite in rapid imaging maneuver,” Aerosp. Syst., Jul. 2025.
[9] B. Yuan, Z. Meng, and R.-Q. Dong, “Design of anti-unwinding attitude coupling controller for flexible spacecraft using positive position feedback control,” Acta Astronaut., vol. 218, pp. 163–176, May 2024.
[10] M. N. Hasan, Y. Chen, J. Liang, and A. Wen, “Fixed-time fault-tolerant attitude control for flexible spacecraft without angular velocity sensor,” ISA Trans., vol. 146, pp. 87–98, Mar. 2024.
[11] E. Azadi, M. Eghtesad, S. Fazelzadeh, and M. Azadi, “Vibration suppression of smart nonlinear flexible appendages of a rotating satellite by using hybrid adaptive sliding mode/Lyapunov control,” J. Vib. Control, vol. 19, no. 7, pp. 975–991, May 2013.
[12] L. Liu, D. Cao, and X. Tan, “Studies on global analytical mode for a three-axis attitude stabilized spacecraft by using the Rayleigh–Ritz method,” Arch. Appl. Mech., vol. 86, no. 12, pp. 1927–1946, 2016.
[13] P. C. Hughes, “Modal identities for elastic bodies, with application to vehicle dynamics and control,” J. Appl. Mech. Trans. ASME, vol. 47, no. 1, pp. 177–184, 1980.
[14] P. W. Likins, “Dynamics and control of flexible space vehicles,” 1970.
[15] D. Lu and Y. Liu, “Singular formalism and admissible control of spacecraft with rotating flexible solar array,” Chinese J. Aeronaut., vol. 27, no. 1, pp. 136–144, 2014.
[16] A. J. Elliott, A. Nakhaeezadeh Gutierrez, L. Felicetti, and L. Zanotti Fragonara, “In-orbit system identification of a flexible satellite with variable mass using dual Unscented Kalman filters,” Acta Astronaut. (Under Rev., vol. 226, pp. 71–86, Jan. 2025.
[17] O. Wallrapp and S. Wiedemann, “Simulation of deployment of a flexible solar array,” Multibody Syst. Dyn., vol. 7, no. 1, pp. 101–125, 2002.
[18] B. Fufa, C. Zhao-Bo, and M. Wensheng, “Modeling and Simulation of Satellite Solar Panel Deployment and Locking,” Inf. Technol. J., vol. 9, no. 3, pp. 600–604, Mar. 2010.
[19] S. Shahriari, S. Azadi, and M. M. Moghaddam, “An accurate and simple model for flexible satellites for three-dimensional studies,” J. Mech. Sci. Technol., vol. 24, no. 6, pp. 1319–1327, 2010.
[20] J. C. Brannan and C. R. Carignan, “Modeling flexible-body dynamics in real-time robotic systems used in satellite servicing simulations,” AIAA Model. Simul. Technol. Conf., 2013.
[21] W. Xu, D. Meng, Y. Chen, H. Qian, and Y. Xu, “Dynamics modeling and analysis of a flexible-base space robot for capturing large flexible spacecraft,” Multibody Syst. Dyn., vol. 32, no. 3, pp. 357–401, 2014.
[22] B. Baghi, M. Kabganian, R. Nadafi, and E. Arabi, “Three-axis attitude stabilization of a flexible satellite using non-linear PD controller,” Trans. Inst. Meas. Control, vol. 40, no. 2, pp. 591–605, 2018.
[23] M. Tahmasebi and S. M. Esmailzadeh, “Modeling and co-simulating of a large flexible satellites with three reaction wheels in ADAMS and MATLAB,” Int. J. Dyn. Control, vol. 6, no. 1, pp. 79–88, 2018.
[24] A. Stolfi, P. Gasbarri, and M. Sabatini, “A parametric analysis of a controlled deployable space manipulator for capturing a non-cooperative flexible satellite,” Acta Astronaut., vol. 148, pp. 317–326, 2018.
[25] D. Zhang, J. Luo, and J. Yuan, “Dynamics modeling and attitude control of spacecraft flexible solar array considering the structure of the hinge rolling,” Acta Astronaut., vol. 153, pp. 60–70, 2018.
[26] H. Soleimani and M. َAzimi, “Modeling and Simulation of a Flexible Spacecraft Solar Panels Deployment Mechanism with Yoke Driven Assembly,” J. Sp. Sci. Technol., vol. 13, no. 4, pp. 37–48, 2020.
[27] G. Lu, J. Zhou, G. Cai, L. Lv, and G. Fang, “Active vibration control of a large space antenna structure using cable actuator,” AIAA J., vol. 59, no. 4, pp. 1457–1468, 2021.
[28] Z. J. Shahbazzadeh, R. Vatankhah, M. Eghtesad, and N. Assadian, “Development and verification of a flexible tethered satellite system model considering the fuel slosh,” Multibody Syst. Dyn., vol. 56, no. 3, pp. 289–312, Nov. 2022.
[29] G. He and D. Cao, “Dynamic Modeling and Attitude–Vibration Cooperative Control for a Large-Scale Flexible Spacecraft,” Actuators, vol. 12, no. 4, 2023.
[30] G. Tagliani, M. Mancini, and E. Capello, “Attitude Control System Design for Multibody Flexible Spacecraft,” Proc. Am. Control Conf., vol. 2023-May, pp. 4820–4825, 2023.
[31] J. Zhang, P. Wu, Q. Han, X. Wei, and Y. Duan, “Dynamic Behavior of Satellite and Its Solar Arrays Subject to Large-Scale Antenna Deployment Shock,” Aerospace, vol. 11, no. 5, 2024.
[32] F. Gao, J. Li, and G. Sun, “Efficient and accurate flexible multibody dynamics modeling for complex spacecraft with integrated control applications,” Acta Astronaut., vol. 219, pp. 818–825, 2024.
[33] M. Liu, Q. Liu, C. Yue, and H. Li, “Prescribed performance fault-tolerant attitude control for flexible spacecraft under limited communication network,” IET Control Theory Appl., vol. 17, no. 11, pp. 1566–1577, 2023.
[34] S. Di Gennaro, “Passive attitude control of flexible spacecraft from quaternion measurements,” J. Optim. Theory Appl., vol. 116, no. 1, pp. 41–60, 2003.
[35] M. Rivandi, M. Mirshams, and M. Zarourati, “Design and Implementation of a Balance System for the CubeSat Attitude Determination and Control Tabletop Simulator,” J. Sp. Sci. Technol., vol. 16, no. 1, pp. 75–88, May 2023.
[36] M. Zarourati, M. Mirshams, and M. Tayefi, “Designing an adaptive robust observer for underactuation fault diagnosis of a remote sensing satellite,” Int. J. Adapt. Control Signal Process., vol. 37, no. 11, pp. 2812–2834, Nov. 2023.
[37] M. Zarourati, M. Mirshams, and M. Tayefi, “Active underactuation fault-tolerant backstepping attitude tracking control of a satellite with interval error constraints,” Adv. Control Appl. Eng. Ind. Syst., vol. 6, no. 3, Sep. 2024.
[38] B. Wie, Space Vehicle Dynamics and Control, Second Edition. Reston ,VA: American Institute of Aeronautics and Astronautics, 2008.
[39] M. Zarourati, M. Mirshams, and M. Tayefi, “Attitude path design and adaptive robust tracking control of a remote sensing satellite in various imaging modes,” Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng., vol. 237, no. 9, pp. 2166–2184, Jul. 2023.