جستجوی مقالات مرتبط با کلیدواژه « nonlinear dynamics inversion » در نشریات گروه « مکانیک »

Undoubtedly, the flight control system is one of the most important parts of an aeronautical vehicles that has duty of stability and achieve good performance in execution of commands. In flight control according to nonlinear dynamics, time varying and structural and parametric uncertainties of aeronautical vehicles, various control approaches use to achieve stability, good performance and reduce the effect of the uncertainties and modeling error. In this paper, autopilot software design were developed using nonlinear dynamics inversion controller to landing a UAV in two stages. Also, with using DSP hardware and CPU TMS320F28335, nonlinear dynamics inversion autopilot software were implemented and tested to real time PIL stage. Finally, nonlinear six-degree-of-freedom simulation results at real-time, confirm proper performance of implementation.