Journal
INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL
Volume 30, Issue 6, Pages 2515-2532Publisher
WILEY
DOI: 10.1002/rnc.4897
Keywords
adaptive control; adding a power integrator; finite-time control; fixed-time control; spacecraft attitude tracking
Funding
- Fundamental Research Funds for the Central Universities of China [2019B01114]
- National Natural Science Foundation of China [61903123]
- Natural Science Foundation of Jiangsu Province [BK20170303, BK20190165]
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In this article, the fixed-time attitude tracking problem for rigid spacecraft is investigated based on the adding-a-power-integrator control technique. First, a fixed-time attitude tracking controller is designed to guarantee fixed-time convergence of tracking errors. Then, by considering the presence of random disturbance and actuator faults, an adaptive fault-tolerant attitude tracking controller is designed to guarantee tracking errors converge to a residual set of zero in a fixed time. The complete bounds on settling time are derived independently of initial conditions. The simulation results illustrate the highly precise and robust attitude control performance obtained by using the proposed controllers.
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