Line-of-Sight Control in Airborne Radar Reconnaissance System
碩士 === 國立交通大學 === 機械工程系所 === 94 === Radar is a device of using electromagnetic waves to detect the presence of the target and extract its location and relative velocity. The airborne radar deviates from its predicted trajectory by pilot-induced maneuvers, atmospheric gusts disturbance and structural...
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ndltd-TW-094NCTU54890752016-05-27T04:18:36Z http://ndltd.ncl.edu.tw/handle/66068451020045522697 Line-of-Sight Control in Airborne Radar Reconnaissance System 機載雷達偵照系統之視線控制 Kan-Yao Chung 張淦垚 碩士 國立交通大學 機械工程系所 94 Radar is a device of using electromagnetic waves to detect the presence of the target and extract its location and relative velocity. The airborne radar deviates from its predicted trajectory by pilot-induced maneuvers, atmospheric gusts disturbance and structural vibrations, and will decrease the detection efficiency of radar. In order to improve the problem, we have to compensate the motion uncertainty of aircraft and correct the motion deviation of radar. The purpose of the thesis is to implement the antenna stabilization system of airborne radar. By setting up a two-axis gimbal mechanism on the antenna pedestal, we can compensate the changing attitudes of aircraft and stabilize the antenna line-of-sight in a designated earth-fixed location. Algorithm used for line-of-sight control generates commands to stabilize and point antenna. The gyroscope and encoders are taken as the sensors of feedback signals in this system. PID controller is developed to minimize tracking error and improve system performance. Wei-Hua Chieng 成維華 2006 學位論文 ; thesis 51 en_US |
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碩士 === 國立交通大學 === 機械工程系所 === 94 === Radar is a device of using electromagnetic waves to detect the presence of the target and extract its location and relative velocity. The airborne radar deviates from its predicted trajectory by pilot-induced maneuvers, atmospheric gusts disturbance and structural vibrations, and will decrease the detection efficiency of radar. In order to improve the problem, we have to compensate the motion uncertainty of aircraft and correct the motion deviation of radar. The purpose of the thesis is to implement the antenna stabilization system of airborne radar. By setting up a two-axis gimbal mechanism on the antenna pedestal, we can compensate the changing attitudes of aircraft and stabilize the antenna line-of-sight in a designated earth-fixed location. Algorithm used for line-of-sight control generates commands to stabilize and point antenna. The gyroscope and encoders are taken as the sensors of feedback signals in this system. PID controller is developed to minimize tracking error and improve system performance.
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author2 |
Wei-Hua Chieng |
author_facet |
Wei-Hua Chieng Kan-Yao Chung 張淦垚 |
author |
Kan-Yao Chung 張淦垚 |
spellingShingle |
Kan-Yao Chung 張淦垚 Line-of-Sight Control in Airborne Radar Reconnaissance System |
author_sort |
Kan-Yao Chung |
title |
Line-of-Sight Control in Airborne Radar Reconnaissance System |
title_short |
Line-of-Sight Control in Airborne Radar Reconnaissance System |
title_full |
Line-of-Sight Control in Airborne Radar Reconnaissance System |
title_fullStr |
Line-of-Sight Control in Airborne Radar Reconnaissance System |
title_full_unstemmed |
Line-of-Sight Control in Airborne Radar Reconnaissance System |
title_sort |
line-of-sight control in airborne radar reconnaissance system |
publishDate |
2006 |
url |
http://ndltd.ncl.edu.tw/handle/66068451020045522697 |
work_keys_str_mv |
AT kanyaochung lineofsightcontrolinairborneradarreconnaissancesystem AT zhānggànyáo lineofsightcontrolinairborneradarreconnaissancesystem AT kanyaochung jīzàiléidázhēnzhàoxìtǒngzhīshìxiànkòngzhì AT zhānggànyáo jīzàiléidázhēnzhàoxìtǒngzhīshìxiànkòngzhì |
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