利用单频GPS接收机和整数模糊约束进行精确运动定位

J. Pinchin, C. Hide, D. Park, Xiaoqi Chen
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引用次数: 18

摘要

在这项工作中,提出了一个系统,将提供载波相位精度定位和两轴姿态测量仅使用三个低成本,单频,GPS接收机。这样的系统将在对成本、重量和功耗要求最低的平台上得到应用;例如微型无人机(UAV)。系统提供的六种状态测量可用于其他传感器数据的地理参考或平台本身的导航。该贡献旨在利用姿态确定系统中获得的双差分整数模糊度知识,提高平台定位时整数模糊度解决过程的成功率。因此,系统的鲁棒性和“解决时间”将得到改善。众所周知,在姿态确定环境中使用基线长度或几何约束可以显著提高整数模糊成功率,特别是在使用低成本单频接收机的情况下。研究表明,这样的约束可能会将成功率提高到接近100%的水平。这些限制条件已被证明可以使低成本的GPS接收机成为一种有效的姿态确定系统。在这项工作中,使用了一个双接收机姿态确定系统与第三基础接收机提供两轴姿态和位置测量。利用姿态确定系统的双差分整数模糊度知识,在搜索包含第三个接收机时产生的整数模糊度时减少候选数。当这些模糊性得到解决时,就可以确定漫游(姿态)接收机与基准接收机之间的未知基线并获得相对位置。定位阶段的约束减小了两个粗纱接收机之间不相关误差的影响。这种好处主要体现在使用低质量的接收机时,由于暴露在高动态环境中,高斯噪声会加剧。然而,在大多数应用中,两个粗纱接收器之间的基线长度可能不允许多径误差的去相关,因此这仍然会产生不利影响。通过将低成本系统与安装在车辆试验台上的高档Novatel SPAN集成GPS/INS系统进行比较,验证了该算法的实际性能。测试是在一个天空视野良好的地区和距离基站3公里以内进行的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Precise kinematic positioning using single frequency GPS receivers and an integer ambiguity constraint
In this work a system is proposed which will provide carrier phase accuracy positioning and two axis attitude measurements using only three low cost, single frequency, GPS receivers. Such a system will find application on platforms where minimal cost, weight and power consumption is critical; for example the mini-unmanned aerial vehicle (UAV). The six state measurements provided by the system may be used in the georeferencing of other sensor data or in the navigation of the platform itself. This contribution aims to increase the success rate of the integer ambiguity resolution process when positioning the platform by utilising knowledge of the double differenced integer ambiguities obtained in an attitude determination system. The robustness and 'time to solution' of the system will thus be improved. It is well known that the use of baseline length or geometry constraints in the attitude determination environment may significantly increase the integer ambiguity success rate, particularly where low cost, single frequency receivers are used. It has been shown that such constraints may increase the success rate to a level approaching 100%. Such constraints have been proven to allow the low cost GPS receiver to become an effective attitude determination system. In this work a two receiver attitude determination system is used with a third base receiver to provide both two axis attitude and position measurement. Knowledge of the double differenced integer ambiguities from the attitude determination system is used to reduce the number of candidates during the search for the integer ambiguities arising when the third receiver is included. When these ambiguities are resolved the unknown baselines between the roving (attitude) receivers and base receiver may be determined and the relative position obtained. The constraint in the positioning stage reduces the effect of uncorrelated errors between the two roving receivers. The benefits of this are observed primarily when using low quality receivers with considerable Gaussian noise exacerbated by exposure to highly dynamic environments. It is likely however that in most applications the baseline length between the two roving receivers will not allow the decorrelation of the multipath error and consequently this will still have a detrimental effect. Real world performance of the algorithm is examined by comparing the low cost system to a high grade Novatel SPAN integrated GPS/INS installed on a vehicle test bed. Tests are performed in an area with good sky view and within 3 km of the base station.
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