Abstract
The target mid-class UAV system used in this study consists of three types of power sources operating simultaneously. These power sources are designed and constructed to share the same operation voltage range and connect to the power bus without additional converters or controllers. The flight test of the target UAV system was conducted for 22.13 hours after the take-off at 20:53 on June 21, 2012. The power sources successfully supplied the propulsion power required during the test flight. In addition, the power simulation was conducted and validated against the flight test results proving that the dynamic behavior of each power source can be properly predicted.
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