Power Unit Test System For Small Unmanned Aerial Vehicle
A test system is proposed,which can be applied to processes of designing,commissioning and other tests for the power unit of unmanned aerial vehicles (UAV).The working principle,software/hardware design and key technologies of this system are specifically introduced.Reliability of various functions of the system is examined and assessed through repeated engine tests,which indicates that,the system can control the engine stably and the data measured can reflect changes in parameters authentically.This system,meeting all requirements for performance testing,commissioning and maintenance of the engine,is suitable for the process of designing,commissioning and other tests for power units of small aircrafts.
UAV power unit engine test-bed test system
Deng Zhao Luo Jian Xu Yang Lin Hui Wu Liaoni
School of Physics and Mechanical & Electrical Engineering Xiamen University Xiamen, China
国际会议
重庆
英文
419-422
2015-12-19（万方平台首次上网日期，不代表论文的发表时间）