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UAV Propulsion Analysis System with Reconfigurable Controller Feature

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In this paper, a custom measuring system for propulsion units of multi-rotor UAV is presented. Designed solution provides measurements of thrust, rotational speed and power consumption of popular electric propulsion systems consisting of BLDC motor, electronic speed controller (ESC) and various propellers. The method is applicable to both single and twin (coaxial) configurations of rotors. Thanks to the use of a precision 6-axis force/torque sensor and sensorless method of speed measurement it is possible to record performance of propulsion with convenient PC software. The system is equipped with complete galvanic isolation between power and sensory circuits. A unique feature of presented solution is the possibility of remote reconfiguration of various controllers, governing speed or thrust of the propeller. Possible applications of the presented test rig are: estimating the performance of UAV design (flight time, power consumption, payload capabilities), mathematical modelling of electric propulsion and analysis of faulty states of rotor operation.
Wydawca
Rocznik
Strony
171--173
Opis fizyczny
Bibliogr. 11 poz., rys., wykr.
Twórcy
autor
autor
autor
  • Institute of Control and Information Engineering Poznań University of Technology 3A Piotrowo St., 60-965 Poznań, Poland, adam.bondyra@put.poznan.pl
autor
  • Institute of Control and Information Engineering Poznań University of Technology 3A Piotrowo St., 60-965 Poznań, Poland, przemyslaw.gasior@put.poznan.pl
autor
Bibliografia
  • [1] Federal Aviation Administration: FAA Aerospace Forecasts, online access 15.01.2017.
  • [2] Hossain M., Krouglicof N.: Propeller dynamometer for small Unmanned Aerial Vehicle, CCECE 2010, Calgary, AB, 2010, pp. 1-5.
  • [3] Theys B., Dimitriadis G., Hendrick P., De Schutter J.: Influence of propeller configuration on propulsion system efficiency of multi-rotor Unmanned Aerial Vehicles, 2016 Intern. Conference on Unmanned Aircraft Systems (ICUAS), Arlington, VA, 2016, pp. 195-201.
  • [4] Bondyra A., Gardecki S., Gąsior P., Giernacki W.: Performance of coaxial propulsion in design of multi-rotor UAVs. Advances in Intelligent Systems and Computing, Vol. 440, 2016, pp. 523-531.
  • [5] Rahnamai K.: Quadrotor drones thrust measurement apparatus, 2016 IEEE Aerospace Conference, Big Sky, MT, 2016, pp. 1-6.
  • [6] Sharf I. et al.: Ground effect experiments and model validation with Draganflyer X8 rotorcraft, 2014 International Conference on Unmanned Aircraft Systems (ICUAS), Orlando, FL, 2014.
  • [7] Gąsior P., Bondyra A., Gardecki S., Giernacki W., Kasiński A.: Thrust estimation by fuzzy modeling of coaxial propulsion unit for multirotor UAVs. In: Multisensor Fusion and Integration for Intelligent Systems (MFI), IEEE Intern. Conf. on, 2016, pp. 418-423.
  • [8] Bondyra A., Gardecki S., Gąsior P.: Distributed control system for multirotor aerial platforms. Measurement Automation Monitoring, vol. 61, no. 07, 2015, pp. 343-346.
  • [9] Bondyra A., Gardecki S., Gąsior P., Kasiński A.: Falcon: A compact multirotor flying platform with high load capability. Advances in Intelligent Systems and Computing, vol. 351, 2015, pp. 35-44.
  • [10] Fręchowicz A., Heyduk A.: Speed and current measurements in control systems for low-speed BLDC motors, online access 09.03.2017
  • [11] STMicroelectronics: AN1946: Sensorless BLDC motor control and BEMF sampling methods with ST7MC, online access 09.03.2017
Uwagi
PL
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-3e3c11cf-580a-4447-a5c5-84f1efac6a93
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