DC 欄位 |
值 |
語言 |
DC.contributor | 光機電工程研究所 | zh_TW |
DC.creator | 蔡易軒 | zh_TW |
DC.creator | I-Hsuan Tsai | en_US |
dc.date.accessioned | 2016-7-15T07:39:07Z | |
dc.date.available | 2016-7-15T07:39:07Z | |
dc.date.issued | 2016 | |
dc.identifier.uri | http://ir.lib.ncu.edu.tw:444/thesis/view_etd.asp?URN=103327005 | |
dc.contributor.department | 光機電工程研究所 | zh_TW |
DC.description | 國立中央大學 | zh_TW |
DC.description | National Central University | en_US |
dc.description.abstract | 本論文目的為開發能自動追蹤具有定位資訊之飛行體的移動式雲台使用的姿態控制系統,使用3DPrint製成的雲台機構為姿態致動器,並整合重力計、地磁計、陀螺儀數據判定姿態。以GPS為基準,探測位於空中50至200公尺處的飛行體,並進行雲台對飛行體之指向。研究已開發完成系統之機構、驅動電路及控制軟體,並設計雲台追蹤性能測試實驗流程。 | zh_TW |
dc.description.abstract | The purpose of this paper is to develop the attitude control system to automatically track the flying object with the location-based information to use cradle head, the use of 3DPrint agency cradle head made the gesture of the actuator, and the integration of gravimetric, magnetic, gyroscope data determined attitude. GPS-reference probe located in the air flying object at 50-200 meters, and use the cradle head to point to the of the flying object . Research has completed the development of the institutional system, the drive circuit and control software, and cradle head tracking performance test design process. | en_US |
DC.subject | 雲台 | zh_TW |
DC.subject | 姿態控制 | zh_TW |
DC.subject | gps訊號 | zh_TW |
DC.subject | 卡門濾波器 | zh_TW |
DC.subject | 指向控制 | zh_TW |
DC.subject | PTZ | en_US |
DC.subject | Attitude Control | en_US |
DC.subject | gps signal | en_US |
DC.subject | kalman filter | en_US |
DC.subject | Pointing Control | en_US |
DC.title | 飛行體自動追蹤移動雲台之開發及研究 | zh_TW |
dc.language.iso | zh-TW | zh-TW |
DC.type | 博碩士論文 | zh_TW |
DC.type | thesis | en_US |
DC.publisher | National Central University | en_US |