Accession Number : ADA307294
Title : Computer Simulation of an Unmanned Aerial Vehicle Electric Propulsion System.
Descriptive Note : Master's thesis,
Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA
Personal Author(s) : Yourkoski, Joel
PDF Url : ADA307294
Report Date : MAR 1996
Pagination or Media Count : 122
Abstract : There has been a substantial increase in the use of electric propulsion systems in Unmannned Aerial Vehicles (UAVs). However, this area of engineering has lacked the benefits of a dynamic model that could be used to optimize the design. configurations and flight profiles. The Naval Research Laboratory (NRL) has accurate models for the aerodynamics associated with UAVs. Therefore the proposed electric propulsion model would use the torque and RPM requirements generated by the aerodynamic model and provide an accurate representation of the desired UAV electric propulsion system. This thesis reports on the development of such a model. The model is adaptive in the sense that motor and battery parameters can be altered by the user to reflect systems currently in use or those considered for future systems. Not only will the simulation model accurately reflect the operating conditions of the motor and battery during the mission, but different flight profiles with the same configuration can be evaluated in terms of efficiency based on the Percent Battery Capacity Used (PBCU) at the end of the mission. This Electric Propulsion Simulator is part of a larger NRL project intended to design and deliver UAVs to the Naval Service over the next few years.
Descriptors : *COMPUTERIZED SIMULATION, *SYSTEMS ENGINEERING, *UNMANNED, *AIRCRAFT MODELS, *ELECTRIC PROPULSION, COMPUTER PROGRAMS, AERODYNAMIC CONFIGURATIONS, SIMULATORS, OPTIMIZATION, MODELS, DYNAMICS, ACCURACY, EFFICIENCY, THESES, ENGINEERING, MISSIONS, USER NEEDS, NAVAL RESEARCH, NAVAL RESEARCH LABORATORIES, FLIGHT PATHS, MOTORS, TORQUE, ELECTRIC BATTERIES.
Subject Categories : Pilotless Aircraft
Computer Programming and Software
Electric and Ion Propulsion
Distribution Statement : APPROVED FOR PUBLIC RELEASE