Aircraft Control System Synthesis Using Sampled Data

• Main Authors: Zhi-Fang Wang, 王志方
• Other Authors: Jenq-Tzong H. Chan
• Format: Others
• Language: zh-TW
• Published: 2000
• Online Access: http://ndltd.ncl.edu.tw/handle/59356135190046019690

碩士 === 國立成功大學 === 航空太空工程學系 === 88 === We have made an attempt to redesign the flight controller for an aircraft in flight, by using a data-based controller synthesis technique. The data needed for the controller design will be obtained through an in flight open-loop system test. Computation of the controller will be performed in real time at the completion of the open-loop test, and while the aircraft remains airborne. Computer simulation of the proposed task on a simulator model of the F-16 fighter will suggest that the task can be accomplished with a reasonable closed-loop system performance. This thesis will address this task in detail, including the results and the drawn conclusions of the simulations.