Desgin and Test of UAV Navigation and Control System

• Main Authors: Chen Chung Kuo, 郭承忠
• Other Authors: C.D.Yang
• Format: Others
• Language: zh-TW
• Published: 2000
• Online Access: http://ndltd.ncl.edu.tw/handle/65963586341074767825

碩士 === 國立成功大學 === 航空太空工程學系 === 88 === For an Unmanned Aerial Vehicles (UAV) which endures long distance flight as out of sight，the autonomous flight system is the key to the all functions。Most missions will be completely done and controlled by on-board computer which lays on UAV system。On-board computer is in charge of a lot of work such as communicating with various sensors、recording / building data system、executing all algorithms、upload/download information、、、etc；in other words，on-board computer like our visualizing pilot who has all abilities to handle all things like to increase the plane stability、know where he is、、、etc。The study aims to develop a flight control system that can improve security and stability of UAV。And in the future，we will add another engine control、guidance and navigation laws and auto taking off 、、、for UAV and make our UAV has really complete autonomous flight system。In the paper，we got the dynamics of UAV by various aerodynamics data in trim state，and then designed the control laws by our specifications for UAV。Finally，we put the whole equipment on UAV and test the controller 。