TWO STAGE ESTIMATION OF FLIGHT PARAMETERS USING GNSS MEASUREMENTS

机译：利用GNSS测量法对飞行参数进行两阶段估算

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In this study, two-stage estimation of aircraft's position and velocity by Global Navigation Satellite System (GNSS) algorithm is presented. In first stage, the distances between the GNSS satellites and aircraft (pseudoranges) and the radial velocities are measured. By this GNSS generated data, an equation system for aircraft is presented and solved. In the second stage, the solutions of the firs stage are improved by Kalman Filtering process.

机译：在这项研究中，提出了通过全球导航卫星系统（GNSS）算法对飞机的位置和速度进行两阶段估计。在第一阶段，测量GNSS卫星和飞机之间的距离（伪距）和径向速度。通过该GNSS生成的数据，提出并求解了飞机的方程组。在第二阶段，通过卡尔曼滤波过程改进了第一阶段的解。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20050523-25; Saint Petersburg(RU)》|2005年|P.188-189|共2页
会议地点 Saint Petersburg(RU)
作者
Ch.M.Hajiyev; M.I. Berberoglu;
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作者单位

Istanbul Technical University, Faculty of Aeronautics and Astronautics, Istanbul, Turkey;

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会议组织
原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
global navigation satellite system; kalman filter; two-stage estimation;

机译：全球导航卫星系统；卡尔曼滤波；两阶段估计;

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TWO STAGE ESTIMATION OF FLIGHT PARAMETERS USING GNSS MEASUREMENTS

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