Disturbance-observer-based attitude control under input nonlinearity
نویسندگان
چکیده
A disturbance observer-based control scheme is proposed in this paper to deal with the attitude stabilization problems of spacecraft subjected external disturbances, parameter uncertainties, and input nonlinearities. Particularly, approach addresses dead-zone issue, a non-smooth nonlinearity affiliated that significantly increases controller design difficulties. novel nonlinear observer (NDO) developed, which relaxes strong assumption conventional NDO disturbances should be constants or varying slow rates. After that, special integral sliding mode (ISMC) combined achieve asymptotic convergence system states. Simulations are performed presence time-varying justify effectiveness scheme.
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ژورنال
عنوان ژورنال: Transactions of the Institute of Measurement and Control
سال: 2021
ISSN: ['0142-3312', '1477-0369']
DOI: https://doi.org/10.1177/0142331221997204