| 摘要 |
The present invention relates to an unmanned aerial vehicle flight control software verification method and, more particularly, to an unmanned aerial vehicle flight control software verification method which includes an error transmitting step (S100) of inputting a preset error to a test board of a control unit from a target board of an external input unit, a function inspecting step (S200) of inspecting a function due to the inputted error by testing a system of flight control software to receive the error through the error transmitting step (S100), and a result outputting step (S300) of monitoring a function inspecting result value according to the function inspecting step (S200). [Reference numerals] (AA) Start; (BB) End; (S100) Error transmitting step; (S200) Function inspecting step; (S300) Result outputting step |
