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Matrices obtained by solving the LMI.

Version 3 2025-10-01, 11:46
Version 2 2024-10-08, 14:02
Version 1 2024-10-08, 13:59
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posted on 2025-10-01, 11:46 authored by Huu Thien NguyenHuu Thien Nguyen, Ionela Prodan, Fernando A. C. C. Fontes
<p dir="ltr">These are the matrices obtained by solving the LMI in Chapter 6 of the PhD thesis "Optimization-Based Control Design for Challenging Maneuvers in Nonholonomic Vehicles", and the manuscript "Nonlinear Model Predictive Control Trajectory Tracking for a Fixed-Wing UAV in a Deep-Stall and Perching Landing Maneuver with Guaranteed Stability".</p><p dir="ltr">*Updated October 1, 2025: we have added the matrices obtained with different values of \epsilon, as well as the time-varying \Upsilon_1(t), \Upsilon(t), and the solving time. </p>

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Motion planning and control for Variable-Geometry UAV operation in a cluttered environment.

Fundação para a Ciência e Tecnologia

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UPWind-ATOL : An Airborne Wind Energy System with Automatic Takeoff and Landing capabilities

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