THE USE OF MATHEMATICAL MODELING TO DETERMINE THE NEED CONFIGURATION OF UNMANNED AIRCRAFT HAVING A VARIABLE STRUCTURE IN FLIGHT

A. L. Kartashev, A. S. Pantileev

Abstract


A balancer control in conjunction with the classical aerodynamic controls will significantly reduce the landing distance. We find the  equations of motion both taking into account a movable load and without it, for unmanned aerial vehicle having a variable  structure in flight.

Keywords


differential equations of motion, variable structure, unmanned aerial vehicle

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