Evidence map›Paper›PMID 41171777›Full record

ArticlePloS one2025

Robust adaptive control with lumped model uncertainty and wind disturbance estimation for airship trajectory tracking.

Muhammad Wasim, Ahsan Ali, Faisal Saleem, Inam Ul Hasan Shaikh, Jamshed Iqbal

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In one paragraph

Article in PloS one, 2025. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Not yet cited in PubMed.

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1 · What the graph read from it

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2 · The registry

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3 · Its place in the literature

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4 · The record

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5 · Who and what money

Authors and funding

5 authors.

Muhammad WasimDepartment of Aeronautics and Astronautics Engineering, Institute of Space Technology, Islamabad, Pakistan.
Ahsan AliDepartment of Electrical Engineering, University of Engineering and Technology, Taxila, Pakistan.
Faisal SaleemDepartment of Measurements and Control Systems, Silesian University of Technology, ul. Akademicka 16, Gliwice, Poland.
Inam Ul Hasan ShaikhDepartment of Electrical Engineering, University of Engineering and Technology, Taxila, Pakistan.ORCID https://orcid.org/0000-0002-6509-5763
Jamshed IqbalSchool of Digital and Physical Sciences, Faculty of Science and Engineering, University of Hull, United Kingdom.ORCID https://orcid.org/0000-0002-0795-0282

Funding

No grant is acknowledged in the PubMed record.

6 · The paper itself

Abstract

The robotic airship can be used as an aerostatic platform for many potential applications, for example, communication, hovering payload deliveries, data-gathering for research studies, etc. These applications require a fully autonomous perspective of an airship. One of the important aspects of airship autonomy is trajectory tracking control. An airship has complex and uncertain nonlinear dynamics which pose a major challenge for designing a precise trajectory tracking control. This paper addresses the airship trajectory tracking control problem under model uncertainties and wind disturbance. We propose a lumped model uncertainties and wind disturbance estimation approach based on an unscented Kalman filter. The estimated lumped uncertainty is used by the Sliding Mode Controller (SMC) for ultimate control of airship trajectory tracking. This comprehensive algorithm, Unscented Kalman filter-based Sliding Mode Controller (USMC), is used as a robust adaptive control solution to track the desired trajectory. The stability and convergence of the proposed method are investigated using the Lyapunov stability analysis. Simulation results show that the proposed method efficiently tracks the desired trajectory. The method solves the stability, convergence, and chattering problem of SMC without the bound constraint of model uncertainties and wind disturbance.

Indexed as

Models, TheoreticalRoboticsWindAlgorithmsComputer SimulationNonlinear DynamicsUncertainty

Identifiers

PMID41171777
PMCPMC12578223

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Read under generation 80e0d062 · epoch 390. Bibliography from PubMed, PubMed Central and OpenAlex; grants from NIH RePORTER; trial links from ClinicalTrials.gov; estimates, votes and beliefs from the OpenQuestion graph.