Development of fault tolerant integrated INS/RADAR altimeter using adaptive filtration algorithm with the filter gain correction

Ch Hajiyev*

*Corresponding author for this work

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

Abstract

Radar Altimeter, Kalman Filter The fault tolerant integrated navigation system, consisting of radar and inertial altimeters, is presented. The integration is achieved by using an adaptive Kalman filter with the filter gain correction. In the open loop system, the inertial altimeter is the main source of information, and radar altimeter provides discrete aiding data to support the estimations. The performance of the proposed fault tolerant integrated radar/inertial altimeter in case of abrupt faults is examined.

Original languageEnglish
Title of host publication13th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2006 - Proceedings
EditorsVladimir G. Peshekhonov, I.S. Afanasova
PublisherState Research Center of the Russian Federation
Pages175-177
Number of pages3
ISBN (Electronic)5900780627, 9785900780627
Publication statusPublished - 2006
Event13th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2006 - Saint Petersburg, Russian Federation
Duration: 29 May 200631 May 2006

Publication series

Name13th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2006 - Proceedings

Conference

Conference13th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2006
Country/TerritoryRussian Federation
CitySaint Petersburg
Period29/05/0631/05/06

Keywords

  • Inertial navigation
  • Integrated navigation systems

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