Longitudinal Total Energy Control of UAS

Описание

A discussion on the derivation, implementation, and response of the Nonlinear Total Energy Control System (Nonlinear TECS) for longitudinal control of an Unmanned Aircraft System (UAS). The Nonlinear TECS response is compared to similar implementations of PID and LQR control on the system. This implementation and derivation is based on the work done by Matthew Argyle and Randal Beard in their work "Nonlinear Total Energy Control for the Longitudinal Dynamics of an Aircraft" and derivation credit should be given to their work.