摘要(英) |
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. |
參考文獻 |
[1] UAV Collaborative, http://www.uav-applications.org/
[2] Hennessey, C.,Autonomous control of a scale airplane, Simon Fraser University, 2000.
[3] H. Claus Christmann, Dr. Eric N. Johnson, M. Scott Kimbrell, Dr. Erwan Salaün, D. Michael Sobers, Jr., Major,Institute of Technology, USAF* Georgia Georgia Tech Aerial Robotics Team International Aerial Robotics Competition Entry Girish Chowdhary, 2009
[4] Federation of American Scientists, http://www.fas.org/irp/program/collect/docs/TUAV-CONOPS.htm
[5] 王唯訓,自建學生衛星地面站開發及測試 (一) ,國立中央大學光機電工程研究所,2009
[6] Y. S. Suh, “Attitude Estimation Using Low Cost Accelerometer and Gyroscope”, The 7th Korea-Russia International Symposium on Science and Technology, Vol.2, 423-427, 2003.
[7] 王嘉,次軌道任務用立方衛星姿態控制系統開發, 國立中央大學光機電工程研究所,2014
[8] GAO Xian-zhong, HOU Zhong-xi† , WANG Bo, ZHANG Jun-tao ,Quaternion-based Kalman filter and its performance analysis in integrated navigation
[9] 陳志明,王惠南,劉海穎,全角度歐拉角與四元數轉換研究,南京航空航天大學自動化學院,南京(210016)
[10] 彭國祐 李守誠 洪兆宇 王振宇,六加速儀機制結合GPS導航應用,2005
[11] 江仁宏,立方衛星無線通訊系統開發,國立中央大學光機電工程研究所,2015
[12] 謝銘峰,GPS/DGPS與慣性導航系統之整合研究,國立交通大學,1995
[13] 鄭期元,整合 GNSS 與 INS 量測資訊的 地平面運動軌跡估測,國立交通大學,2013 |