| GPS辅助姿态计算的捷联陀螺罗经实现 |
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| 引用本文： | 冯爱国,徐晓苏.GPS辅助姿态计算的捷联陀螺罗经实现[J].上海海事大学学报,2010,31(4):17-22. |
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| 作者姓名： | 冯爱国 徐晓苏 |
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| 作者单位： | 1. 南通航运职业技术学院,航海系,江苏,南通,226010;东南大学,微惯性仪表与先进导航技术教育部重点实验室,南京,210096
2. 东南大学,微惯性仪表与先进导航技术教育部重点实验室,南京,210096 |
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| 基金项目： | 国家自然科学基金 (60874092, 50575042)；总装备部预研项目(51309060402，51309020503)；原国防科学技术工业委员会基础科研项目(C1420080224)；航空科学基金(20080869009) |
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| 摘 要： | 为给船舶提供可靠的航向信息，提高系统集成化及数字化程度，降低设计成本及机械复杂度，提出利用四元数法对GPS及捷联惯性器件输出的数据进行解算，设计基于捷联惯导系统姿态计算的免施矩罗经方法.通过分析以GPS及捷联惯性器件数据确定初始姿态矩阵、利用罗经法进行精对准及修正角速率计算、惯性器件数据坐标系转换、角增量计算、四元数更新、姿态矩阵更新、姿态计算等系列算法，给出用串口采集及处理GPS数据和微惯性器件数据的方案，设计算法实现的软件流程.仿真分析表明，系统启动时间短，输出结果稳定，误差在商船允许范围内，虚拟仪表显示实时、准确.
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| 关 键 词： | 捷联惯导系统 姿态解算 GPS参数 四元数 陀螺罗经 |
| 收稿时间： | 7/5/2010 11:10:03 AM |
| 修稿时间： | 2010/8/12 0:00:00 |
Strapdown gyrocompass design based on GPS assisted attitude calculation |
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| FENG Aiguo,XU Xiaosu.Strapdown gyrocompass design based on GPS assisted attitude calculation[J].Journal of Shanghai Maritime University,2010,31(4):17-22. |
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| Authors: | FENG Aiguo XU Xiaosu |
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| Institution: | Department of Navigation, Nantong Shipping College,1 |
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| Abstract: | In order to provide ships with reliable heading information and improve the integration and digital level of the system, and reduce the cost and mechanical complexity, a calculation method with GPS and strapdown inertial instrument output data using quaternion method is proposed, and a torque free compass based on Strapdown Inertial Navigation System(SINS) attitude algorithm is designed. By analyzing several algorithms, such as initial attitude matrix determination with GPS and strapdown inertial instrument data, fine alignment and calculation of angular rate correction using gyrocompass, coordinates transformation of inertial instrument data, calculation of angle increment, quaternion, attitude matrix updating and attitude calculation, the scheme of collecting GPS and micro inertial instrument data through serial port is presented, and the procedures of algorithm are designed. The simulation results indicate that the system has short start time and stable output, the error is within the acceptable range of commercial ships, and the virtual instrument has real time and accurate display. |
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| Keywords: | strapdown inertial navigation system attitude algorithm GPS data quaternion gyrocompass |
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