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