在全球轨道导航卫星系统中使用 SPP 方法提高飞机定位精度

Q2 Engineering Archives of Transport Pub Date : 2024-03-13 DOI:10.61089/aot2024.v0s1gv25
K. Krasuski, A. Ciećko, G. Grunwald, M. Kirschenstein
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引用次数: 0

摘要

本文介绍了一项研究的结果,该结果显示了根据全球轨道导航卫星系统(GLONASS)中的 SPP(单点定位)解决方案确定飞机位置坐标的准确性。为此,本文开发并实施了一种位置误差修正算法,作为描述定位精度的参数。所提议的算法使用为单个 GNSS(全球导航卫星系统)接收器确定的位置误差值,并将其线性组合,以确定飞机的定位精度。该算法使用线性系数作为全球导航卫星系统接收器跟踪的格洛纳斯卫星数量的反函数。在使用 Cessna 172 飞机围绕 Dęblin军用机场进行飞行测试期间,对拓普康 HiPer Pro 和 Javad Alpha 大地测量接收器记录的全球轨道导航卫星系统卫星数据进行了测试。使用 RTKLIB v.2.4.3 和 Scilab v.6.0.0 软件进行了导航计算。根据所进行的测试发现,对于单个 Topcon HiPer Pro 和 Javad Alpha 接收机,位置误差高达 ±11.4 米。然而,通过对这两个接收机使用位置误差修正算法,全球轨道导航卫星系统的定位精度高达 ±3.6 米。所开发的算法可将所有 BLh(B-纬度,L-经度,h-椭球高度)坐标的位置误差减少 60-80%。论文展示了在 GPS(全球定位系统)导航系统中测试和实施所提出的 SPP 解决方案数学算法的可能性。在这种情况下,对于所有 BLh 坐标,GPS SPP 解决方案的位置误差范围为 -0.9 米至 +0.9 米。结果表明,在航空运输中应用全球轨道导航卫星系统和全球定位系统非常重要。这项工作中使用的算法也可应用于航空运输和导航中的其他全球导航卫星系统(如伽利略(欧洲导航卫星系统)或北斗(中国导航卫星系统))。
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Improving positioning accuracy of aircraft using SPP method in GLONASS system
The paper presents the results of a study showing the accuracy of the determination of aircraft position coordinates based on the SPP (Single Point Positioning) solution in the GLONASS (Globalnaja Navigatsionnaya Sputnikovaya Sistema) system. For this purpose, the paper develops and implements an algorithm for the correction of position errors as parameters describing positioning accuracy. The proposed algorithm uses position error values determined for a single GNSS (Global Navigation Satellite Systems) receiver, which are joined in a linear combination to determine the positioning accuracy of the aircraft. The algorithm uses linear coefficients as an inverse function of the number of GLONASS satellites being tracked by the GNSS receiver. The developed algorithm was tested for GLONASS satellite data recorded by Topcon HiPer Pro and Javad Alpha geodetic receivers, during a flight test carried out with a Cessna 172 aircraft around the military airport in Dęblin. Navigation calculations were carried out using RTKLIB v.2.4.3 and Scilab v.6.0.0 software. On the basis of the tests carried out, it was found that for single Topcon HiPer Pro and Javad Alpha receivers, position errors were up to ±11.4 m. However, by using the position error correction algorithm for both receivers, GLONASS positioning accuracy is up to ±3.6 m. The developed algorithm reduces position errors by 60-80% for all BLh (B- Latitude, L- Longitude, h- ellipsoidal height) coordinates. The paper shows the possibility of testing and implementing the proposed mathematical algorithm for the SPP solution in a GPS (Global Positioning System) navigation system. In this case the position errors from the GPS SPP solution range from -0.9 m to +0.9 m for all BLh coordinates. The obtained results showed that application the GLONASS and GPS system in air transport is important. The algorithm used in this work can also be applied to other global GNSS navigation systems (e.g. Galileo (European Navigation Satellite system) or BeiDou (Chinese Navigation Satellite System))  in air transport and navigation.
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来源期刊
Archives of Transport
Archives of Transport Engineering-Automotive Engineering
CiteScore
2.50
自引率
0.00%
发文量
26
审稿时长
24 weeks
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