Autonomous Flight Control and System Integration For Unmanned Helicopter

• Main Authors: WU,ZHONG-DA, 吳忠達
• Other Authors: 黃意勛
• Format: Others
• Language: zh-TW
• Published: 2019
• Online Access: http://ndltd.ncl.edu.tw/handle/tstqec

碩士 === 高苑科技大學 === 電子工程研究所 === 107 === Unmanned helicopters with [high] mobility, can be suspended and fixed landing with landing site demand for small features, the global countries for the UAV in the military field invest a lot of research and development and application of investment, UAV technology makes the application of the type has been changed from Traditional reconnaissance evolved to carry out the task of attacking ground targets, and vertical take-off and landing vehicles are the next major goal of UAV technology. To achieve this goal, with vertical takeoff and landing of the vehicle will be the necessary technology for the development of unmanned aerial vehicles. Based on PixFalcon flight control computer, this study completed the system integration work, and then realized the following 7 aspects: stabilize, altitude hold, hovering, position hold, guided, RTL and automatic flight mode. In this experiment, we will conduct integrated flight test experiments and collect data to achieve unmanned helicopter autonomous flight control and system integration..