发明名称 ATTITUDE CONTROL METHOD USING TARGET TRACK APPROXIMATION
摘要 A satellite attitude control method using target track approximation is provided to adjust the attitude of a satellite by making a task plan quickly if the attitude of the satellite needs to be regulated at a track, due to plural photographing regions. A satellite attitude control method using target track approximation includes the steps for inputting coordinate information of at least one target point(401); generating a target track passing all input target points by selectively utilizing an approximation method using a polynomial expression on the basis of coordinate information of the input target points, an approximation method using a Fourier series, and an approximation method using neural network(402,403); and checking the position of a satellite at the present track, calculating an attitude track for the target track by using the present position of the satellite and coordinate information of the target point, and then applying the calculated attitude track to a satellite attitude control operation(404,405).
申请公布号 KR100793058(B1) 申请公布日期 2008.01.10
申请号 KR20060094396 申请日期 2006.09.27
申请人 ELECTRONICS AND TELECOMMUNICATIONS RESEARCH INSTITUTE 发明人 JEONG, SEONG KYUN;LEE, SANG UK;KIM, JAE HOON
分类号 G01S13/06 主分类号 G01S13/06
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