Dual Quaternion Based Fault-tolerant Control for Spacecraft Tracking with Finite-time Convergence

HY Dong (Harbin Institute of Technology, China), QL Hu (Beihang University, China), MI Friswell (Swansea University) & GF Ma (Harbin Institute of Technology, China)

IEEE Transactions on Control Systems Technology, Vol. 25, No. 4, July 2017, pp. 1231-1242

Abstract

Results are presented for a study of dual-quaternion-based fault-tolerant control for spacecraft tracking. First, a six-degrees-of-freedom dynamic model under a dual-quaternion-based description is employed to describe the relative coupled motion of a target-pursuer spacecraft tracking system. Then, a novel fault-tolerant control method is proposed to enable the pursuer to track the attitude and the position of the target even though its actuators have multiple faults. Furthermore, based on a novel time-varying sliding manifold, finite-time stability of the closed-loop system is theoretically guaranteed, and the convergence time of the system can be given explicitly. Multiple-task capability of the proposed control law is further demonstrated in the presence of disturbances and parametric uncertainties. Finally, numerical simulations are presented to demonstrate the effectiveness and advantages of the proposed control method.

Paper Availability

This material has been published in the IEEE Transactions on Control Systems Technology, Vol. 25, No. 4, July 2017, pp. 1231-1242, the only definitive repository of the content that has been certified and accepted after peer review. Copyright and all rights therein are retained by IEEE.


Link to paper using doi: 10.1109/TCST.2016.2603070

IEEE Transactions on Control Systems Technology