PARAMETRIC IDENTIFICATION OF INTEGRATED NAVIGATION SYSTEMS IN REAL TIME AND FROM FLIGHT DATA

机译：实时和飞行数据集成导航系统的参数识别

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Problems that arise during use of integrated navigation systems (INS) are considered. The proposed solutions permit us to take into account any changes in dynamic and accuracy characteristics of sensors by means of the appropriate coefficients of the models of errors. Under actual conditions of INS operation, the determination of current values of the parameters of the models of sensors and of an estimation filter rely on identification procedures. The results of full-scale experiments are given, which corroborate the expediency of parametric identification of the models of INS errors in real time and from flight data.

机译：考虑了在使用集成导航系统（INS）期间出现的问题。所提出的解决方案使我们能够通过误差模型的适当系数考虑到传感器动态和精度特性的任何变化。在INS运行的实际条件下，确定传感器模型和估计滤波器模型的参数的当前值取决于识别过程。给出了全面实验的结果，证实了实时和从飞行数据中对INS错误模型进行参数识别的便利性。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20050523-25; Saint Petersburg(RU)》|2005年|P.109-118|共10页
会议地点 Saint Petersburg(RU)
作者
A.V. Chernodarov; A. Yu. Platonov; V. L. Budkin; V.P.Golikov; S.V.Larionov; S.L. Bulgakov; Yu.P. Mikheenkov; A.P. Patrikeev;
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作者单位

Zhukovsky Air Force Engineering Academy, 3, Planetnaya St., 125190, Moscow, Russia;

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原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
integrated navigation systems; state control; sensors; model of errors; parametric identification;

机译：组合导航系统;状态控制;传感器;误差模型;参数识别;

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专利

1. Parametric Identification and Diagnosis of Integrated Navigation Systems in Bench Test Process [J] . Ilya Prokoshev, Alexander Chernodarov International Journal Information Theories and Applications . 2008,第3期

机译：台架试验过程中组合导航系统的参数识别与诊断
2. SOLUTION OF A PROBLEM ON PARAMETRIC IDENTIFICATION OF THE STOCHASTIC STATE VECTOR IN THE FLIGHT VEHICLE NAVIGATION SYSTEM [J] . V. A. Pogorelov, K. Yu. Yakovlev, V. V. Ryzhov Russian Aeronautics . 2004,第4期

机译：飞行器导航系统中随机状态矢量的参数识别问题的解决
3. Integrated Big Data Analytics Technique for Real-Time Prognostics, Fault Detection and Identification for Complex Systems [J] . Chinedu I. Ossai Infrastructures . 2017,第4期

机译：集成的大数据分析技术，用于复杂系统的实时预测，故障检测和识别
4. PARAMETRIC IDENTIFICATION OF INTEGRATED NAVIGATION SYSTEMS IN REAL TIME AND FROM FLIGHT DATA [C] . A.V. Chernodarov, A. Yu. Platonov, V. L. Budkin, Saint Petersburg International Conference on Integrated Navigation Systems . 2005

机译：实时和飞行数据中集成导航系统的参数识别
5. In-flight detection of errors for enhanced aircraft flight safety and vertical accuracy improvement using digital terrain elevation data with an inertial navigation system, global positioning system and radar altimeter. [D] . Gray, Robert Anthony. 1999

机译：使用惯性导航系统，全球定位系统和雷达高度计的数字地形高程数据，在空中进行错误检测，以提高飞机的飞行安全性和垂直精度，从而提高飞行效率。
6. Real-time comparative evaluation of bioMerieux VITEK MS versus Bruker Microflex MS two matrix-assisted laser desorption-ionization time-of-flight mass spectrometry systems for identification of clinically significant bacteria [O] . Wafaa Jamal, M John Albert, Vincent O Rotimi 2014

机译：两种基质辅助激光解吸电离飞行时间质谱系统bioMerieux VITEK MS与Bruker Microflex MS的实时比较评估用于鉴定临床上重要的细菌
7. Parametric Identification and Diagnosis of Integrated Navigation Systems in Bench Test Process [O] . Prokoshev Ilya, Chernodarov Alexander 2008

机译：台架试验过程中组合导航系统的参数识别与诊断
8. Design and Analysis of Integrated Navigation Systems Using Real INS and GPS Data [R] . Evans, C. D. 1994

机译：基于真实INs和Gps数据的组合导航系统设计与分析

PARAMETRIC IDENTIFICATION OF INTEGRATED NAVIGATION SYSTEMS IN REAL TIME AND FROM FLIGHT DATA

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