OPTIMAL REAL-TIME INTEGRATION OF SATELLITE AND INERTIAL SYSTEMS DATA

机译：卫星和惯性系统数据的最佳实时集成

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摘要

The problem of optimal estimation of the trajectory of a carrier for an inertial system and a satellite receiver is studied. We assume that measurement noises are locally stationary and carrier oscillations spectrum is narrow-band with respect to the passband of the inertial sensor; no other assumptions are required. The optimal estimate of the trajectory is evaluated in the spectral form by using the Baudot-Shannon procedure.

机译：研究了惯性系统和卫星接收机的最优航迹估计问题。我们假设测量噪声相对于惯性传感器的通带而言是局部静止的，并且载波振荡频谱是窄带的。无需其他假设。通过使用Baudot-Shannon过程以谱形式评估轨迹的最佳估计。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20060529-31; Saint Petersburg(RU)》|2006年|P.159-160|共2页
会议地点 Saint Petersburg(RU)
作者
S.N. Podkorytov;
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作者单位

OAO HC , 196066, St. Petersburg, Moskovskiy pr., 212;

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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
real-time data processing; optimal filtering; navigation system;

机译：实时数据处理；最佳过滤；导航系统;

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1. Performance assessment of a low-cost inertial measurement unit based ultra-tight global navigation satellite system/inertial navigation system integration for high dynamic applications [J] . Feng Qin, Xingqun Zhan, Lei Zhan Radar, Sonar & Navigation, IET . 2014,第7期

机译：基于低成本惯性测量单元的超紧密全球导航卫星系统/惯性导航系统集成的性能评估
2. Solution to the problem of the close integration of satellite and inertial platform navigation systems [J] . Pogorelov V. A., Sokolov S. V. Cosmic research . 2015,第6期

机译：解决卫星与惯性平台导航系统紧密结合的问题
3. Optimal processing of information from inertial an satellite navigation systems by analysis after flight [J] . Kharin E. G., Maslennikov V. G., Vavilova N. B., Радиотехника . 2001,第1期

机译：飞行后通过分析对惯性卫星导航系统的信息进行最佳处理
4. OPTIMAL REAL-TIME INTEGRATION OF SATELLITE AND INERTIAL SYSTEMS DATA [C] . S.N. Podkorytov Saint Petersburg International Conference on Integrated Navigation Systems . 2006

机译：卫星和惯性系统数据的最佳实时集成
5. High precision navigation integrating satellite information -GPS- and inertial system data [D] . Cunha, Telmo Reis. 2002

机译：集成卫星信息-GPS和惯性系统数据的高精度导航
6. Implementation and Analysis of Tightly Coupled Global Navigation Satellite System Precise Point Positioning/Inertial Navigation System (GNSS PPP/INS) with Insufficient Satellites for Land Vehicle Navigation [O] . Yue Liu, Fei Liu, Yang Gao, 2018

机译：陆地车辆导航用卫星不足的紧密耦合全球导航卫星系统精确点定位/惯性导航系统（GNSS PPP / INS）的实现和分析
7. Dynamics and real-time optimal control of satellite attitude and satellite formation systems [O] . Yan Hui 2006

机译：卫星姿态和卫星编排系统的动力学和实时最优控制
8. A real-time algorithm for integrating differential satellite and inertial navigation information during helicopter approach [R] . Hoang, TY 1994

机译：一种在直升机进近过程中积分差分卫星和惯性导航信息的实时算法

OPTIMAL REAL-TIME INTEGRATION OF SATELLITE AND INERTIAL SYSTEMS DATA

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