Development of the Motion Control and Simulation of the Aircraft Attitude by Using the NI myRIO

• Main Author: 顏睦家
• Other Authors: 陳啟川 博士
• Format: Others
• Language: zh-TW
• Published: 2016
• Online Access: http://ndltd.ncl.edu.tw/handle/37532997001709168130

碩士 === 逢甲大學 === 航太與系統工程學系 === 104 === It has been a long time since the development of Stewart platform, and the platform also has been widely used in a variety of mechanic structure, such as flight simulator and other fields. The thesis utilizes the NI myRIO, which is developed by National Instrument company, as a control core to build the auxiliary system for flight instruction. By changing different parameters, a flight simulation system with motion control is finally realized. The calculations of the elongation for each actuator are performed with the attitude and heading information received from the electronic compass and accelerometers integrated inside NI myRIO and the algorithm of the Inverse Kinematics(IK). To achieve the purpose of motion simulation and attitude control, the output PWM signals sent to servo motors for driving the Stewart Platform to desired attitude/location are also generated by control core.