Two stage estimation of flight parameters using GNSS measurements

Ch M. Hajiyev, M. I. Berberoglu

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

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.

Original languageEnglish
Title of host publication12th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2005
EditorsI.S. Afanasova, Vladimir G. Peshekhonov
PublisherState Research Center of the Russian Federation
Pages188-189
Number of pages2
ISBN (Electronic)5900780597, 9785900780597
Publication statusPublished - 2005
Event12th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2005 - Saint Petersburg, Russian Federation
Duration: 23 May 200525 May 2005

Publication series

Name12th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2005

Conference

Conference12th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2005
Country/TerritoryRussian Federation
CitySaint Petersburg
Period23/05/0525/05/05

Keywords

  • Global navigation satellite system
  • Kalman filter
  • Two-stage estimation

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