查詢結果分析
相關文獻
頁籤選單縮合
題名 | 六加速儀慣性導航系統硬品實現與驗證=The Realization and Verification of Six-Accelerometer INS |
---|---|
作者 | 洪兆宇; 李守誠; Hung, Chao-yu; Lee, Sou-chen; |
期刊 | 黃埔學報 |
出版日期 | 20080300 |
卷期 | 54(工程科學類) 2008.03[民97.03] |
頁次 | 頁9-16 |
分類號 | 440.98 |
語文 | chi |
關鍵詞 | 慣性導航系統; 慣性量測單元; 電子單元; 計算單元; INS; Inertial measurement unit; Electric unit; Computed unit; |
中文摘要 | 六加速儀慣性導航系統(Six-Accelerometer INS)乃應用六顆加速儀感測值計算航具位置、速度與姿態變化之慣性導航系統,可取代傳統陀螺儀式慣性導航系統。慣性導航系統係由慣性量測單元(Inertial Measurement Unit IMU)、電子單元(Electric Unit EU)及計算單元(Computed Unit EU)等三個次要系統所組成,本論文運用此一系統架構,將六加速儀慣性導航系統硬體實現化,並實際架設於一小型載具上驗證理論,經驗證結果,六加速儀慣性導航系統可提供載具導航使用,未來可應用於自動駕駛與無人飛行載具(UAV)之研究。 |
英文摘要 | The six-accelerometer INS can calculate the direction, velocity and position of a motive vehicle through the measurement outputs of six accelerometers. It is able to instead of the traditional gyro-accelerometer INS. An inertial navigation system contains three components which are inertial measurement unit (IMU), electric unit (EU) and computed unit (CU). There are two topics in this paper. First, the paper is through proposed architecture to realize six-accelerometer INS hardware. Another is the six-accelerometer theory be verified through an experiment of a moving INS vehicle. The result of verification show that the six-accelerometer INS can apply to navigation. The novel method of six-accelerometer INS would be considered in auto-pilot and UAV design for the future application. |
本系統之摘要資訊系依該期刊論文摘要之資訊為主。