吉林大学学报(地球科学版) ›› 2019, Vol. 49 ›› Issue (3): 857-864.doi: 10.13278/j.cnki.jjuese.20190010
赵肖, 郑孝诚, 焦健, 于平, 董向欣
Zhao Xiao, Zheng Xiaocheng, Jiao Jian, Yu Ping, Dong Xiangxin
摘要: 航磁补偿飞行中,飞机姿态变化产生的磁场严重影响航磁数据精度。为了补偿飞机产生的磁干扰,基于Tolles-Lawson方程建立补偿模型,其中关键是计算方向余弦值;采用Leach提出的基于三轴磁通门解算方向余弦方法建立航磁补偿系统;依据当地水平坐标系与飞机坐标系之间的旋转关系,建立了机载三轴磁通门数据的理论模型解算方向余弦,从而验证了该补偿方法的有效性。将该方法运用到云南某实验场地的航磁补偿数据中,并选择标准差作为评价补偿效果的指标,得到补偿质量满足规范要求,说明基于磁通门估计的航磁补偿方法是有效的。
中图分类号:
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