衝擊放大式微重力計硬體在迴路測試

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姓名

簡文淵(WUN-YUAN JIAN) 查詢紙本館藏

畢業系所

光機電工程研究所

論文名稱

衝擊放大式微重力計硬體在迴路測試
(Hardware in the loop testing of the Impact Enlarged Microgravity Meter.)

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檔案

[Endnote RIS 格式]

[Bibtex 格式]

[相關文章]

[文章引用]

[完整記錄]

[館藏目錄]

至系統瀏覽論文 ( 永不開放)

摘要(中)

本論文的目的為開發硬體模擬在迴路測試在進行正式實測前，驗證衝擊放大式微重力計軟硬體之功能，由於不易取得真實微重力環境下的加速度，因此利用已開發之電腦動態模擬軟體，模擬在微重力環境下的加速度感測數據，依照此數據產生替代MEMS加速度計之輸出訊號，以模擬真實訊號，藉以激發微重力計之硬體控制系統的功能，以確認控制系統的軟硬體對於受測環境的反應之正確性。

摘要(英)

Micro gravity environment is difficult to obtain, if is desirable to verify the functionality of a microgravity meter during its development before its real tests in the micro gravity environment. A computerized mems accelerator emulator is developed to generate its electric signals lased on the simulation results of the sensing function of the Impact Enlarged Micro gravity Meter in a real test. The emulated signals until stimulate the control system of the micro gravity meter to confirm its correct response to the real impact data of would be real micro gravity test.

關鍵字(中)

★ 微重力計
★ 硬體在迴路

關鍵字(英)

論文目次

摘要 I
ABSTRACT II
致謝 III
目錄 IV
圖目 V
表目 VI
第一章引言 1
1.1 研究目的與動機 1
1.2 文獻回顧 2
1.3 研究構想 6
1.4 論文章節 6
第二章理論背景 7
2.1 機械系統動態 7
2.2 彈性碰撞 8
2.3 數學模型 10
2.4 B2BBUS原理 16
第三章系統設計 19
3.1 系統功能方塊 19
3.2 狀態機械 22
3.3 硬體電路 31
3.4 系統具體實現 33
第四章衝擊放大微重力計硬體在迴路測試 36
第五章結論 45

參考文獻

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指導教授

葉則亮

審核日期

2015-7-30

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