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  • 學位論文

微機電慣性量測組件驗證環境之設計

Test Bed Development for MEMS Inertial Measurement Unit

指導教授 : 蕭照焜

摘要


本論文研究並設計ㄧ個自製微機電慣性量測組件驗證的環境。主要包含加速儀、陀螺儀的測試方法、無線資料傳輸系統的開發以及測試流程的建立:基於實驗平台的運動機構,分別設計出適合於加速儀及陀螺儀測試的動作,藉由理論的分析分別找出加速儀及陀螺儀於該動作下所應量得的理論值,並透過無線數據傳輸系統進行實驗數據的擷取,由實驗數據的分析來了解各感測元件的狀態並計算出角速度(加速度)與電壓之間的關係,最後再與使用手冊所提供的數據相互比較,以確定實驗結果的可靠。 我們針對所設計的測試動作建立最佳的實驗流程:加速儀測試、單軸陀螺儀測試及三軸陀螺測試;由單軸陀螺儀測試的結果我們可得角速度與電壓的關係式,接著進行三軸陀螺儀測試,將實驗結果代入我們所求出的關係式並與理論值進行比較,以了解實驗所得的關係式之適用性。

並列摘要


In this thesis, we developed a test bed for the in-house designed low cost MENS inertial measurement unit (IMU). The test system consists of a four-axis platform, a motion control computer, and a wireless data transmission system. We designed an adaptable test motion for the accelerometers and gyroscopes based on the mechanical structure of the platform. A promising test procedure for the accelerometer and gyroscope tests using the test bed is proposed. The relation between the measured value (AD count) and the angular velocity is established for each individual MEMS gyroscope. A mathematic framework is also derived to verify the performance of the three-axis gyros (three single-axis MEMS gyros installed perpendicularly to provide three axes measurement). Experiment and analysis results are provided to show the effectiveness of the test bed.

參考文獻


[2] Leland R.P., “ Lyapunov based adaptive control of a MEMS gyroscope”, American Control Conference. Proceedings of the Volume 5, pp.3765-3770, 2002.
[8] ADP3335 Data Sheet, Analog Devices, Inc., 2004.
[9] nRF905 Data Sheet, Nordic Semiconductor ASA, 2006.
[10] PIC18FXX2 Data Sheet, Microchip, Inc., 2002.
[14] Donald McLean, “Automatic Flight Control Systems”, Prentice-Hall, 1990.

被引用紀錄


林昱亨(2010)。以微機電飛行資訊量測系統為基礎之飛行姿態計算:擴展式卡曼濾波之實務探討〔碩士論文,淡江大學〕。華藝線上圖書館。https://doi.org/10.6846/TKU.2010.00351
吳宗興(2008)。以微機電系統為基礎之飛行資訊量測組件設計與製作〔碩士論文,淡江大學〕。華藝線上圖書館。https://doi.org/10.6846/TKU.2008.00908

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