@article{Hu2018ContinuousFA, title={Continuous Finite-Time Attitude Control for Rigid Spacecraft Based on Angular Velocity Observer}, author={Qinglei Hu and Boyan Jiang}, journal={IEEE Transactions on Aerospace and Electronic Systems}, year={2018}, volume={54}, pages={1082-1092} }

- Published 2018 in IEEE Transactions on Aerospace and Electronic…
DOI:10.1109/TAES.2017.2773340

This paper addresses the problem of designing an angular velocity observer and an output feedback attitude controller with finite-time convergence and disturbances for spacecraft. First, two new concepts of finite-time stability are proposed and defined as the local fast-finite-time stability and the fast-finite-time uniformly ultimately boundness, which… CONTINUE READING

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