Gaussian process-based state derivative estimator with temporal input in incremental flight control design

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In this paper, a state derivative estimation technique is proposed using a derivative of Gaussian process regression method and applied to an incremental dynamics -based controller. The state derivative estimates of interest are with respect to time, and to obtain them, the temporal index array is used for Gaussian process state input. Using a Gaussian process, assumptions such as numerical differentiation of the state, parametric basis functions common in adaptive approaches, and the use of upper -bound information of the state derivative commonly used in robust methods are avoided. The proposed approach is compared with the backward difference formula (BDF) differentiator, first -order low-pass filter, second -order low-pass filter, and high -order sliding mode differentiator. Monte Carlo simulation with 1000 runs is performed under four different noise level measurement scenarios. The proposed Gaussian process -based differentiator with temporal index input resulted in better robustness and adaptability in state derivative estimation with similar or better performance.
Publisher
ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
Issue Date
2024-05
Language
English
Article Type
Article
Citation

AEROSPACE SCIENCE AND TECHNOLOGY, v.148

ISSN
1270-9638
DOI
10.1016/j.ast.2024.109070
URI
http://hdl.handle.net/10203/322465
Appears in Collection
AE-Journal Papers(저널논문)
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