Nonlinear control of a tilt augmented multi-rotor UAV with a fixed maximum convergence rate in presence of Inertia uncertainties

Control Engineering Practice 2026

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Authors: Sathyanarayanan Seshasayanan, Soumya Ranjan Sahoo
DOI: 10.1016/j.conengprac.2025.106747
Cited by: 1
References: 30

Fields of Study & Subjects

Adaptive Control of Nonlinear Systems Aeroelasticity and Vibration Control Aerospace and Aviation Technology

Publication details

Journal / source
Control Engineering Practice
Publisher
Elsevier BV
Volume
168
Pages
106747–106747
Publication date
3 January 2026
Language
EN