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FY-2 Meteorological Satellite Attitude Solving Method Under Area Scan Mode
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摘要: 针对风云二号气象卫星区域扫描模式下姿态求解问题，提出了分别基于区域观测图像、姿态预报和粗-精姿态关系模型3种不同的卫星姿态求解方法，并分析了它们的适用条件。利用FY-2E卫星获取的2013年7月8—14日的图像进行模拟分析，姿态计算结果表明：利用基于区域观测图像方法求解的姿态对区域观测云图进行定位，误差保持在2.5个红外像元以内，该方法适用于连续区域观测情况；利用基于预报的姿态求解方法对未来24 h内区域观测云图进行定位，平均误差达到1个红外像元，该方法适用于临时启动区域观测时前24 h的区域云图定位。利用粗-精姿态关系模型方法求解的姿态对区域观测云图进行定位，最大误差为4.9个红外像元，前24 h平均误差为3.6个红外像元，该方法可以在无精姿态数据时对区域观测图像进行应急定位。Abstract: Area observation is realized by the geostationary meteorological satellites of the United States and Europe. The timeliness of satellite observation is greatly improved, and an instance can be accomplished within several minutes. Geostationary meteorological satellites of FY-2 series have the capability of specific area observation, but due to the strip image navigation problem, the area observation of FY-2 satellites is not put into operational use. Therefore, the attitude determination technology of FY-2 satellites' area observation is studied and 3 solving methods are proposed, which are based on area images, attitude prediction, and the relation model between crude and precise attitude.The attitude determination method based on area images uses area images to calculate satellite attitude directly. This method is applicable to the condition that area images can be obtained continuously. When area images are accumulated for twenty-four hours, the method navigates the area image with the attitude gained by the method based on area images. The navigation deviation is in 2.5 infrared pixels. FY-2 satellite receives full disk images under normal observation mode, and receives high-frequency area images under emergency observation mode when special weather occurs. When using the attitude to navigate satellite image at the beginning of area observation, the image navigation accuracy maybe not ideal because the area images quantity is not enough. On this occasion, the attitude solving method based on attitude prediction can be used. With this method, the average deviation of image navigation can be reduced to 1 pixel. Based on the precise attitude which is gained through full disk images, this method predicts the future satellite attitude according to the variety rules of attitude. It is applicable to predict navigation parameter in future 24 hours with mathematics model while precise orbit attitude parameter is obtained. The attitude solving method based on relation model of crude-precise attitude uses the crude attitude which is calculated from telemetry data and the relation between the latest crude-precise attitude, and estimates precise attitude from the crude attitude which is calculated in real time. Using the attitude gained by this method to navigate the image, the max navigation deviation of area image is 4.9 infrared pixels, and the average deviation of former 24 hours is 3.6 infrared pixels. When precise attitude is not available, the attitude obtained by the method based on relation model of crude-precise attitude can be used to navigate area image during emergency situations.
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图 1 基于区域观测图像的姿态确定方法计算结果和实测结果比较
Fig. 1 Results of attitude determination method based on the observed image region compared with measurements
图 2 基于预报的姿态求解方法计算结果与实测结果比较
Fig. 2 Results of solving attitude based on forecast compared with measurements
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[1] 薛谌彬, 龚建东, 何财福, 等.静止卫星云导风的质量控制及在同化中的应用.应用气象学报, 2013, 24(3):356-364. doi: 10.11898/1001-7313.20130312 [2] 黄勇, 覃丹宇.舟曲泥石流天气过程中云团合并的卫星观测.应用气象学报, 2013, 24(1):87-98. doi: 10.11898/1001-7313.20130109 [3] 刘健, 张里阳.气象卫星高空间分辨率数据的云量计算与检验.应用气象学报, 2011, 22(1):35-45. doi: 10.11898/1001-7313.20110104 [4] 韩秀珍, 吴朝阳, 郑伟, 等.基于水面实测光谱的太湖蓝藻卫星遥感研究.应用气象学报, 2010, 21(6):724-731. doi: 10.11898/1001-7313.20100609 [5] 许健民, 张其松.卫星风推导和应用综述.应用气象学报, 2006, 17(5):574-582. doi: 10.11898/1001-7313.20060515 [6] [2013-07-06]. http://www.eumetsat.int/Home/Main/Satellites/MeteosatSecondGeneration/Services/SP_20100628161215372. [7] 王素娟, 郭强, 许健民.FY-4气象卫星定位用导航星选取方法.应用气象学报, 2010, 21(2):149-156. doi: 10.11898/1001-7313.20100203 [8] Pei C.Attitude determination algorithms for spinning satellites using single antenna GPS receiver and MEMS gyro.Aerospace Science and Technology, 2013, 26(1):10-15. doi: 10.1016/j.ast.2012.02.009 [9] D'Angelo M, Linares R, Crassidis J L.Attitude determination for a small satellite mission.Advances in the Astronautical Sciences, 2012, 144:165-171. https://experts.umn.edu/en/publications/attitude-determination-for-a-small-satellite-mission [10] 谌一夫, 张春玲, 张慧, 等.ZY-3卫星的姿态和轨道模型研究.华中师范大学学报:自然科学版, 2013(3):421-425;430. http://www.cnki.com.cn/Article/CJFDTOTAL-HZSZ201303026.htm [11] Cao L, Yang W W, Chen X Q, et al.The research of micro-satellite attitude determination based on predictive filter.Applied Mechanics and Materials, 2012, 110-116:5413-5419, DOI 10.4028/www.scientific.net/AMM.110-116.5413. doi: 10.4028/www.scientific.net/AMM.110-116.5413 [12] Jiao Y, Wang J, Pan X, et al.Influence analysis of measurement errors in satellite attitude determination based on extended Kalman filter.Aeronautical Journal, 2012, 116(1178):373-389. doi: 10.1017/S0001924000005273 [13] 李鹏, 唐健, 段广仁, 等.基于自适应联邦滤波的卫星姿态确定.中国空间科学技术, 2013(2):67-71. doi: 10.3780/j.issn.1000-758X.2013.06.009 [14] 魏喜庆, 宋申民.基于容积卡尔曼滤波的卫星姿态估计.宇航学报, 2013(2):193-200. http://www.cnki.com.cn/Article/CJFDTOTAL-YHXB201302008.htm [15] 张健, 孙兆伟.粒子滤波在卫星姿态确定中的应用.哈尔滨工业大学学报, 2012(11):31-35. doi: 10.11918/j.issn.0367-6234.2012.11.006 [16] 李于衡, 易克初, 关鹏.地球静止轨道自旋卫星姿态确定及控制策略.飞行器测控学报, 2009, 24(5):19-26. http://www.cnki.com.cn/Article/CJFDTOTAL-YHXB200903023.htm [17] 陈宝林.最优化理论与算法 (第二版).北京:清华大学出版社, 2005:322-328. [18] Lu Feng, Zhang Xiaohu, Xu Jianmin.Image navigation for the FY2 geosynchronous meteorological satellite.Journal of Atmospheric & Oceanic Technology, 2008, 25(7):1149. doi: 10.1175/2007JTECHA964.1 [19] Ahn S J, Rauh W, Cho H S.Orthogonal distance fitting of implicit curves and surfaces.IEEE Trans PAMI, 2002, 24(5):620-638. doi: 10.1109/34.1000237 [20] Cui Y T, Weng J, Reynolds H.Estimation of ellipse parameters using optimal minimum-variance estimator.Pattern Recognition Letter, 1996, 17(3):309-316. doi: 10.1016/0167-8655(95)00114-X [21] Nick B, Robert B, Naoki S.A method to detect and characterize ellipses using the Hough transform.IEEE Trans PAMI, 1999, 21(7):652-657. doi: 10.1109/34.777377 [22] 李于衡, 杨小芹, 关鹏, 等.基于遥测数据的定点自旋卫星姿态选优方法.哈尔滨工业大学学报, 2009, 41(5):175-177. http://www.cnki.com.cn/Article/CJFDTOTAL-HEBX200905044.htm -
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