This article discusses the results of modeling the field control system of an unmanned aerial vehicle (UAV) type of the okeoxopter in the Simintech dynamic simulation environment, where the developed mathematical model was exported, and the control system based on proportional and integral-differentiating (PID) of the regulator was properly. Simulation of the Octoxen control system was completed by exporting the control system developed in the Simulink environment. The described approach to modeling the control system allows you to evaluate the Capter Management System and reproduce the dynamics of the real physical object. At the same time, the simulation of the effects of precession is omitted here, it is assumed that the jet moment of each screw-engine group (NMG) is zero, namely: each NMG has two engines and screws rotating at the same speed in opposite sides. The question of modeling equipment failures is also omitted and it is assumed that the object is only in the air (in normal mode of flight), landing and take-off modes, emergency situations, cargo capture and unloading - in the above model are not implemented, and no question of detailed simulation of sensors, filtering Signals and noise, bending of the frame of the copter and / or screws, work on the proceedable loads, writing the drivers to one or another hardware. The technical result of the application of the algorithm is the design and parametric implementation of the object dynamics model in general and in the amount sufficient to design the flight controller and the ground control panel of the copter.
Quadrocopter, unmanned aerial vehicle, hardware and software system, hardware and software system, math modeling
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