Matrices obtained by solving the LMI.

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".*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.

本数据集包含通过求解博士学位论文"Optimization-Based Control Design for Challenging Maneuvers in Nonholonomic Vehicles"（面向非完整车辆复杂机动的基于优化的控制设计）与研究手稿"Nonlinear Model Predictive Control Trajectory Tracking for a Fixed-Wing UAV in a Deep-Stall and Perching Landing Maneuver with Guaranteed Stability"（带稳定性保证的深失速与栖停着陆机动场景下固定翼无人机（Fixed-Wing UAV）非线性模型预测控制（Nonlinear Model Predictive Control）轨迹跟踪）第6章中的线性矩阵不等式（Linear Matrix Inequality, LMI）所得到的矩阵。*2025年10月1日更新：新增了采用不同ε（epsilon）取值得到的矩阵，以及时变的$Upsilon_1(t)$、$Upsilon(t)$和求解时长。