博碩士論文 105327005 完整後設資料紀錄

DC 欄位 語言
DC.contributor機械工程學系zh_TW
DC.creator林恆安zh_TW
DC.creatorHeng-An Linen_US
dc.date.accessioned2018-7-23T07:39:07Z
dc.date.available2018-7-23T07:39:07Z
dc.date.issued2018
dc.identifier.urihttp://ir.lib.ncu.edu.tw:88/thesis/view_etd.asp?URN=105327005
dc.contributor.department機械工程學系zh_TW
DC.description國立中央大學zh_TW
DC.descriptionNational Central Universityen_US
dc.description.abstract本研究以亥姆霍茲線圈(Helmholtz Coil)開發一個可程式、高解析度的動態磁場模擬艙,利用前饋控制與回饋控制抵銷外部環境磁場的干擾,產生高精度的動態磁場環境,提供磁相關系統執行硬體在迴路測試。磁場的規劃有靜態磁場與動態磁場兩種模式,磁場的輸出範圍為±100000nT。 動態磁場可自行設定衛星軌道與初始姿態,模擬衛星在該軌道中運行的磁場歷程,並接受衛星體受力回饋計算姿態歷程,提供磁致動姿態控制系統驗證,執行硬體在迴路測試;而靜態磁場可以提供磁感測儀器進行校正與性能硬體在迴路測試。zh_TW
dc.description.abstractThis study is to develop a programmable, high-resolution dynamic magnetic field simulator by the Helmholtz Coil, which uses feed-forward control and feedback control to offset the external magnetic field disturbance to make a highly accurate dynamic magnetic field to supply Magnetic systems perform hardware-in-the-loop testing. The magnetic field is planned to have two modes: static magnetic field and dynamic magnetic field. The magnetic field range is +100000nT~-100000nT. The dynamic magnetic field can set the satellite orbit and initial attitude, simulate the magnetic field history of the satellite running in the orbit, and accept the satellite force feedback to calculate the attitude history, provide magnetic actuation attitude control system verification, and hardware-in-the-loop testing. Static magnetic fields can provide magnetic sensor for calibration and hardware-in-the-loop testing.en_US
DC.subject衛星姿態控制zh_TW
DC.subject亥姆霍茲線圈zh_TW
DC.subject硬體在迴路測試zh_TW
DC.subject磁場模擬艙zh_TW
DC.title衛星姿態控制硬體在迴路測試用之磁場模擬艙zh_TW
dc.language.isozh-TWzh-TW
DC.titleThe magnetic field simulation instrument for the hardware-in-the-loop testing of Satellite attitude controlen_US
DC.type博碩士論文zh_TW
DC.typethesisen_US
DC.publisherNational Central Universityen_US

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