发明名称 FLIGHT CONTROL ABILITY TEST SYSTEM OF UNMANED HELICOPTER AND METHOD THEREOF
摘要 A system and a method for evaluating flight control ability of an unmanned helicopter are provided to evaluate objectively the flight control ability of a controller controlling the unmanned helicopter and remove error occurring in evaluation by using location information of the flying unmanned helicopter. An absolute coordinate generator(200) generates absolute coordinates according to time by receiving GPS(Global Positioning System) data from a satellite(100) and calculates correction data for correcting the error of the absolute coordinates according to a time gap. The unmanned helicopter(300) generates relative coordinates by receiving the GPS data from the satellite. A flight control ability evaluator(400) generates corrected coordinate by receiving the absolute and relative coordinates, and the correction data, and generates corrected flight path coordinates, which are generated based on the relative coordinates at first, correcting the coordinates as much as the correction data according to the time gap. The flight control ability evaluator determines whether the corrected coordinates are escaped from the corrected flight path coordinates over a predetermined range, and determines qualification depending on a determination result. Further, the absolute coordinate generator contains an absolute coordinate generating part, a revision data generating part and a data storing part.
申请公布号 KR20070121864(A) 申请公布日期 2007.12.28
申请号 KR20060056629 申请日期 2006.06.23
申请人 MOOSUNG AVIATION CO., LTD. 发明人 PARK, WILLIAM J;YANG, JUNG MO
分类号 G06Q50/20 主分类号 G06Q50/20
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