Abstract
Under the extensive application of the spacecraft, an adaptive sliding mode fault tolerant controller is proposed for a spacecraft with the actuator effectiveness and external disturbance. In this approach, the attitude fault-tolerant control scheme based on the sliding mode control theory is design to achieve fault-tolerant control and external disturbance rejection. Then, considering the unknown parameters problem of the actuator and disturbance, adaptive methods is introduced to real-time estimate the unknown parameters, which improve the robustness and practicality of the controller. Finally, the stability of the proposed controller is proved based on the Lyapunov theory and the simulation results show the method with strong fault tolerance for spacecraft actuator failure.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Similar content being viewed by others
References
Zou, A.M., Kumar, K.D.: Robust attitude coordination control for spacecraft formation flying under actuator failures. J. Guid. Control Dyn. 35(4), 1247–1255 (2012)
Boskovic, J.D., Bergstrom, S.E., Mehra, R.K.: Robust integrated flight control design under failures, damage, and state–dependent disturbances. J. Guid. Control Dyn. 28(5), 902–917 (2005)
Godard, Kumar, K.D.: Fault tolerant reconfigurable satellite formations using adaptive variable structure techniques. J. Guid. Control Dyn. 33(3), 969–984 (2010)
Varma, S., Kumar, K.D.: Fault tolerant satellite attitude control using solar radiation pressure based on nonlinear adaptive sliding mode. Acta Astronaut. 66(3–4), 486–500 (2009)
Lee, H., Kim, Y., Kim, H.S.: Satellite attitude control with a modified iterative learning law for the decrease in the effectiveness of the actuator. Int. J. Aeronaut. Space Sci. 11(2), 87–97 (2010)
Noumi, A., Takahashi, M.: Fault tolerant attitude control systems for satellite equipped with control moment gyros. In: AIAA Guidance, Navigation, and Control Conference. AIAA 2013, p. 5119. AIAA, Boston (2013)
Chandrasekar, S., Suresh, S., Sundararajan, N., et al.: An intelligent fault tolerant satellite attitude control system without hardware redundancies. In: 11th International Conference on Control, Automation, Robotics and Vision, pp. 50–56. IEEE, Singapore (2010)
De Ruiter, A.: A fault-tolerant magnetic spin stabilizing controller for the JC2Sat-FFmission. Acta Astronaut. 68, 160–171 (2010)
Li, Z., Yang, X.B., Gao, H.J.: Autonomous impulsive rendezvous for spacecraft under orbital uncertainty and thruster faults. J. Franklin Inst. Eng. Appl. Math. 350, 2455–2473 (2013)
Wei, J.B., Liu, K., Wu, J.J.: Adaptive sliding mode attitude controller for satellites three-axis-stabilized in inertial frame. J. Control Decis. 28(8), 1231–1236 (2013)
Hu, Q.L., Zhang, A.H., Li, B.: Adaptive variable structure fault tolerant control of rigid spacecraft under thruster faults. Acta Aeronautica ET Astronautica Sinica 34(4), 909–918 (2013)
Cai, W., Liao, X.H., Song, Y.D.: Indirect robust adaptive fault-tolerant control for attitude tracking of spacecraft. J. Guid. Control Dyn. 31(5), 1456–1463 (2008)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Switzerland AG
About this paper
Cite this paper
Li, A. et al. (2020). Adaptive Sliding Mode Fault Tolerant Control of Spacecraft with Actuator Effectiveness. In: Xu, Z., Parizi, R., Hammoudeh, M., Loyola-González, O. (eds) Cyber Security Intelligence and Analytics. CSIA 2020. Advances in Intelligent Systems and Computing, vol 1146. Springer, Cham. https://doi.org/10.1007/978-3-030-43306-2_59
Download citation
DOI: https://doi.org/10.1007/978-3-030-43306-2_59
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-43305-5
Online ISBN: 978-3-030-43306-2
eBook Packages: Intelligent Technologies and RoboticsIntelligent Technologies and Robotics (R0)