On the Development of a Flight Control System by Using the sbRIO/FPGA Module
碩士 === 逢甲大學 === 航太與系統工程所 === 98 === The aim of this thesis is to develop an autonomous navigation system for the unmanned aerial vehicle with LabVIEW FPGA module. The onboard computer, NI sbRIO-9631, acquires the data of attitude sensor, GPS receiver, RF module and altimeter through RS-232. At the s...
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ndltd-TW-098FCU052950172016-04-20T04:18:20Z http://ndltd.ncl.edu.tw/handle/09448045846132837312 On the Development of a Flight Control System by Using the sbRIO/FPGA Module 應用sbRIO/FPGA模組於飛行控制系統之建構 Tsung-Hsun Hsieh 謝宗勳 碩士 逢甲大學 航太與系統工程所 98 The aim of this thesis is to develop an autonomous navigation system for the unmanned aerial vehicle with LabVIEW FPGA module. The onboard computer, NI sbRIO-9631, acquires the data of attitude sensor, GPS receiver, RF module and altimeter through RS-232. At the same time, the flight status of the aircraft is analyzed by the flight control software coded by author. After calculating, the instructions will be sent to MiniSSC-II servo controller to command the control surfaces for adjusting the heading and attitude of the aircraft and to guide it to the destination. The aircraft can transmit its status to the ground control station; the ground control station can also send new waypoints back to the aircraft. If the situation of the aircraft is unable to meet the expectation, it will return to the take-off point automatically. The ground control station can command and make it switch to the manual control mode anytime, while the aircraft is within visual range. Chii-Chuan Chen 陳啟川 2010 學位論文 ; thesis 77 zh-TW |
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碩士 === 逢甲大學 === 航太與系統工程所 === 98 === The aim of this thesis is to develop an autonomous navigation system for the unmanned aerial vehicle with LabVIEW FPGA module. The onboard computer, NI sbRIO-9631, acquires the data of attitude sensor, GPS receiver, RF module and altimeter through RS-232. At the same time, the flight status of the aircraft is analyzed by the flight control software coded by author. After calculating, the instructions will be sent to MiniSSC-II servo controller to command the control surfaces for adjusting the heading and attitude of the aircraft and to guide it to the destination. The aircraft can transmit its status to the ground control station; the ground control station can also send new waypoints back to the aircraft. If the situation of the aircraft is unable to meet the expectation, it will return to the take-off point automatically. The ground control station can command and make it switch to the manual control mode anytime, while the aircraft is within visual range.
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author2 |
Chii-Chuan Chen |
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Chii-Chuan Chen Tsung-Hsun Hsieh 謝宗勳 |
author |
Tsung-Hsun Hsieh 謝宗勳 |
spellingShingle |
Tsung-Hsun Hsieh 謝宗勳 On the Development of a Flight Control System by Using the sbRIO/FPGA Module |
author_sort |
Tsung-Hsun Hsieh |
title |
On the Development of a Flight Control System by Using the sbRIO/FPGA Module |
title_short |
On the Development of a Flight Control System by Using the sbRIO/FPGA Module |
title_full |
On the Development of a Flight Control System by Using the sbRIO/FPGA Module |
title_fullStr |
On the Development of a Flight Control System by Using the sbRIO/FPGA Module |
title_full_unstemmed |
On the Development of a Flight Control System by Using the sbRIO/FPGA Module |
title_sort |
on the development of a flight control system by using the sbrio/fpga module |
publishDate |
2010 |
url |
http://ndltd.ncl.edu.tw/handle/09448045846132837312 |
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