An analysis of operation of brushless DC machine used in unmanned aerial vehicle hybrid drive

This paper presents results of a study concerning operating modes of brushless DC machine (BLDCM) used in the hybrid drive designed for unmanned aerial vehicle (UAV). A mathematical model of the machine and a simulation model of the whole drive system are proposed. Structure of the parallel hybrid drive system is discussed. Results of simulations are presented for three different operation modes provided for the machine in the UAV drive system, i.e. engine starting, motoring operation with regulated airscrew speed, and generating operation. Finally, preliminary results of laboratory tests are presented.