Study on Stabilization and Tracking for SOTM
The stabilization and Tracking issue was studied for sOTM,and the low cost M&C system applied open loop stabilization,closed loop tracking and error correcting was put forward based on the analysis for influencing factors on beam attitude control. The method using dynamic inclinometer correcting gyro error based on open loop control was brought forward,in closed loop control,the pointing error was derived from satellite tracking information,and the control structure using tracking information was built,the computer simulation indicates that this method could correct gyro low frequency error effectively.
SOTM open loop closed loop stabilization tracking error correcting.
Guimin Xu Huachun Xu Wei Jin
College of Marine,Northwestern Polytechnical University,710072 Xian,China Xian High-tech Institute,710025 Xian,China
国际会议
2009 9th International Conference on Electronic Measurement & Instruments(第九届电子测量与仪器国际会议 ICEMI2009)
北京
英文
240-244
2009-08-16(万方平台首次上网日期,不代表论文的发表时间)