Abstract: This paper proposes a pitch plane trajectory tacking control solution for suborbital launch vehicles relying on adaptive feedback linearization. Initially, the 2D dynamics and kinematics for ...
Abstract: With the large-scale integration of distributed photovoltaic (PV), the grid condition is gradually presenting as a weak grid. Furthermore., multiple inverters are connected to the end of the ...
A MATLAB implementation of the GARTEUR Research Civil Aircraft Model (RCAM) for nonlinear six-degree-of-freedom flight dynamics simulation, trim analysis, numerical linearization, and state-space ...
We used MATLAB and Simulink and Python. They all work together in a system that can handle many kinds of physics. A fully reproducible reduced-order implementation of the core simulation logic, ...
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