Abstract
Spacecraft need high-precision attitude control according to control instructions when it is in space. Aiming to design an attitude controller for the spacecraft system with multiple rotating components. Firstly, the relative kinematic models are proposed, and attitude dynamics equation of spacecraft which is carrying rotating payload is given by using Lagrange method; Secondly, by introducing the functional equation related to the state variable into the nonsingular sliding mode surface, a new control scheme is designed, and it is theoretically demonstrated that the controller can ensure the stability of spacecraft system based on Lyapunov method. Finally, the numerical simulation and comparative analysis of control methods show that control strategy can not only can guarantee rapidity and stability of spacecraft attitude maneuver, but also can avoid the singularity of traditional sliding mode surface and realize high-precision tracking of expected signal and can also to be demonstrated the superior performance in terms of robustness.
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References
George, V.I., Kamath, B.G., Thirunavukkarasu, I., et al.: Vibration control of flexible spacecraft using adaptive controller. Int. Adv. Sci. Eng. Inf. Technol. 2(1), 2088–5334 (2011). https://doi.org/10.18517/ijaseit.2.1.149
Wang, J., Li, D.X.: Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters, pp. 185–186. Springer, Singapore (2022). https://doi.org/10.1007/978-981-16-5097-0
Cui, M.Y., Xu, S.J., Jia, Y.H.: Flexible spacecraft attitude control based on perturbation method analysis. J. Bei**g Univ. Aeronaut. Astronaut. 36(12), 1387–1391 (2010). https://doi.org/10.13700/j.bh.1001-5965.2010.12.003
Liu, M., Xu, S.J., Han, C.: Direct adaptive attitude tracking control of flexible spacecraft based on backstep** method. Acta Aeronautica et Astronautica Sinica 2034–2037 (2012)
Chen, Z.Y., Huang, J.: Attitude tracking and disturbance rejection of rigid spacecraft by adaptive control. IEEE Trans. Autom. Control 54(3), 600–605 (2009). https://doi.org/10.1109/TAC.2008.2008350
Liu, X.X., Zhang, W.G., Wu, Y., et al.: A different design of robust flight control system based on direct adaptive control. J. Northwest. Polytech. Univ. 26(3), 341–345 (2008). https://doi.org/10.3969/j.issn.1000-2758.2008.03.014
**, E., Sun, Z.W.: Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control. Aerosp. Sci. Technol. 12(4), 324–330 (2008). https://doi.org/10.1016/j.ast.2007.08.001
**ao, B., Hu, Q.L., Zhang, Y.M.: Adaptive sliding mode fault tolerant attitude tracking control for flexible spacecraft under actuator saturation. IEEE Trans. Control Syst. Technol. 20(6), 1605–1612 (2011). https://doi.org/10.1109/TCST.2011.2169796
Eshghi, S., Varatharajoo, R.: Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS). Aerosp. Sci. Technol. 76, 14–26 (2018). https://doi.org/10.1016/j.ast.2018.02.006
Lee, K.W., Singh, S.N.: Three-axis adaptive attitude control of spacecraft using solar radiation pressure. Proc. Inst. Mech. Eng. J. Aerosp. Eng. 229(3), 407–422 (2015)
Lee, K.W., Singh, S.N.: A HigherOrder sliding mode three-axis solar pressure satellite attitude control system. J. Aerosp. Eng. 29(1), 04015019 (2016). https://doi.org/10.1061/(ASCE)AS.1943-5525.0000509
Lu, K.F., **a, Y.Q., Zhu, Z., Basinb, M.: Sliding mode attitude tracking of rigid spacecraft with disturbances. J. Frankl. Inst. 349(2), 413–440 (2012). https://doi.org/10.1016/j.jfranklin.2011.07.019
Zhang, J.R., Zhang, W.T., Zeng, X.Y.: Robust controller design for the attitude control of spacecraft with uncertainty. Trans. Bei**g Inst. Technol. 31(10), 1198–1202 (2011). (in Chinese)
Golestani, M., Esmailzadeh, S., Mobayen, S.: Fixed-time control for high-precision attitude stabilization of flexible spacecraft. Eur. J. Control (2020, to be published). https://doi.org/10.1016/j.ejcon.2020.05.006
Zheng, L., Dong, X.L., Luo, Q., et al.: Robust adaptive sliding mode fault tolerant control for nonlinear system with actuator fault and external disturbance. Math. Probl. Eng. (2019). https://doi.org/10.1155/2019/6349510
Yu, Z.F., Yang, Z.C.: Effects of scan mirror motion on the attitude of three-axis-stabilized geostationary satellite. J. Northwest. Polytech. Univ. 21(1), 87–90 (2003)
Li, Y., Wu, H.Y., Wu, J.: Genetic algorithm PID Self-tuning based on the satellite attitude control. Chin. Space Sci. Technol. 8(4), 66–71 (2007). (in Chinese)
Du, X.P., Hao, G.T., Gao, Y.M.: RBFNN siding mode attitude control method of spacecraft with mobile bodies. Aerosp. Control (05), 61–65 (2012). (in Chinese). https://doi.org/10.3969/j.issn.1006-3242.2012.05.011
Liu, J., Han, C., Zhang, W.: Analysis on disturbance of mobile bodies and compensation control of satellite attitude. Aerosp. Shanghai 23(6), 22–26 (2006). https://doi.org/10.3969/j.issn.1006-1630.2006.06.005
Wu, F., Cao, X.B., Butcher, E., et al.: Dynamics and control of spacecraft with a large misaligned rotational component. Aerosp. Sci. Technol. 87, 207–217 (2019). https://doi.org/10.1016/j.ast.2019.02.029
Zhang, G.W., Wang, F., Chen, J., Li, Y.: Fixed-time sliding mode attitude control of a flexible spacecraft with rotating appendages connected by magnetic bearing. Math. Biosci. Eng. 19(3), 2286–2309 (2022). https://doi.org/10.3934/mbe.2022106
Zhang, G.W., Chen, X.Q., ** sliding mode control for combined spacecraft with nonlinear disturbance observer. In: 2016 UKACC 11th International Conference on Control (CONTROL), pp. 1–6 (2016). https://doi.org/10.1109/CONTROL.2016.7737539
Yu, S.H., Yu, X.H., Shirinzadeh, B., et al.: Continuous finite-time control for robotic manipulators with terminal sliding mode. Automatica 41(11), 1957–1964 (2005). https://doi.org/10.1016/j.automatica.2005.07.001
Hardy, G., Littlewood, J., Polya, G.: Inequalities. Cambridge University Press, Cambridge (1952)
Zhong, C.X., Li, P., Guo, J., et al.: Robust adaptive attitude Manoeuvre control with finite-time convergence for a flexible spacecraft. Trans. Inst. Meas. Control 40(2), 425–435 (2018). https://doi.org/10.1177/0142331216659337
Miao, Y., Wang, F., Liu, M., et al.: Adaptive fast nonsingular terminal sliding mode control for attitude tracking of flexible spacecraft with rotating appendage. Aerosp. Sci. Technol. 93, 105312 (2019). https://doi.org/10.1016/j.ast.2019.105312
Funding
This work is supported by the Science Center Program of National Natural Science Foundation of China (62188101), the National Natural Science Foundation of China (61833009,61690212,51875119,11972130), the Heilongjiang Touyan Team, and the Guangdong Major Project of Basic and Applied Basic Research (2019B030302001).
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Zhang, G., Zhai, H., Guo, H., Liu, M. (2023). Sliding Mode Attitude Control of Flexible Spacecraft with Rotational Components. In: Yan, L., Duan, H., Deng, Y. (eds) Advances in Guidance, Navigation and Control. ICGNC 2022. Lecture Notes in Electrical Engineering, vol 845. Springer, Singapore. https://doi.org/10.1007/978-981-19-6613-2_176
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DOI: https://doi.org/10.1007/978-981-19-6613-2_176
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