Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/92789
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Title: Incremental sliding-mode fault-tolerant flight control
Authors: Wang, X
Van, Kampen, EJ
Chu, Q
Lu, P 
Issue Date: Feb-2019
Source: Journal of guidance, control, and dynamics, Feb. 2019, v. 42, no. 2, p. 244-259
Abstract: This paper proposes a novel control framework that combines the recently reformulated incremental nonlinear dynamic inversion with (higher-order) sliding-mode controllers/observers, for generic multi-input/multi-output nonlinear systems, named incremental sliding-mode control. As compared to the widely used approach that designs (higher-order) sliding-mode controllers/observers based on nonlinear dynamic inversion, the proposed incremental framework can further reduce the uncertainties while requiring less model knowledge. Because the uncertainties are reduced in the incremental framework, theoretical analyses demonstrate that the incremental sliding-mode control can passively resist a wider range of perturbations with reduced minimum possible control/observer gains. These merits are validated via numerical simulations for aircraft command tracking problems, in the presence of sudden actuator faults and structural damage.
Publisher: American Institute of Aeronautics and Astronautics, Inc.
Journal: Journal of guidance, control, and dynamics 
ISSN: 0731-5090
EISSN: 1533-3884
DOI: 10.2514/1.G003497
Rights: © 2018 by Xuerui Wang, Delft University of Technology
This is the peer reviewed version of the following article: Wang, X., Kampen, E. J. V., Chu, Q., & Lu, P. (2019). Incremental sliding-mode fault-tolerant flight control. Journal of guidance, control, and dynamics, 42(2), 244-259 , which has been published in final form at https://doi.org/10.2514/1.G003497
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