Skip to main content
Top

2015 | OriginalPaper | Chapter

117. A Novel In-flight Alignment Algorithm for Airborne Strapdown INS with Assistant of Doppler Radar

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

In order to improve the precision of Doppler and Strapdown inertial navigation system (SINS) integrated navigation system with moving base, an in-flight alignment method is proposed by making an uniform circular motion of the aircraft according to the phenomena avaliable in the Doppler/SINS navigation system tests. The platform error-angles of the SINS can be estimated quickly and the prediction precise can be improved by this method. Experiment verifies the feasibility and validity of this method. Theoretical analysis shows that the steady state limit of the estimation can be highly reduced by proposed method, and the method is valuable for practical application.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Literature
1.
go back to reference Muhammad JA, Ushaq M. A consistent and robust Kalman filter design for in-motion alignment of inertial navigation system. Measurement. 2008;10(2):1–6.MATH Muhammad JA, Ushaq M. A consistent and robust Kalman filter design for in-motion alignment of inertial navigation system. Measurement. 2008;10(2):1–6.MATH
2.
go back to reference Wang X, Guo L. An intelligentized and fast calibration method of SINS on moving base for planed missiles. Aerosp Sci Technol. 2009;4(4):1–8. Wang X, Guo L. An intelligentized and fast calibration method of SINS on moving base for planed missiles. Aerosp Sci Technol. 2009;4(4):1–8.
3.
go back to reference Wang X. Fast alignment and calibration algorithms for inertial navigation system. Aerosp Sci Technol. 2009;4(2):1–6. Wang X. Fast alignment and calibration algorithms for inertial navigation system. Aerosp Sci Technol. 2009;4(2):1–6.
4.
go back to reference Chan GP, Kim K. UKF based In-flight alignment using low cost IMU. AIAA GNCCE. 2006;08(9):1–12. Chan GP, Kim K. UKF based In-flight alignment using low cost IMU. AIAA GNCCE. 2006;08(9):1–12.
5.
go back to reference Wang X, Gong D, Xu L, Shao X. Laser radar based relative navigation using improved adaptive Huber filter. Acta Astronautica. 2011;68(8):1872–80.CrossRef Wang X, Gong D, Xu L, Shao X. Laser radar based relative navigation using improved adaptive Huber filter. Acta Astronautica. 2011;68(8):1872–80.CrossRef
6.
go back to reference Hajiyev C. Fault tolerant integrated radar/inertial altimeter based on nonlinear robust adaptive Kalman filter. Aerosp Sci Technol. 2012;17(7):40–9.CrossRef Hajiyev C. Fault tolerant integrated radar/inertial altimeter based on nonlinear robust adaptive Kalman filter. Aerosp Sci Technol. 2012;17(7):40–9.CrossRef
7.
go back to reference Kim DY, Jeon M. Data fusion of radar and image measurements for multi-object tracking via Kalman filtering. Inform Sci. 2014;27(6):43–9.MathSciNet Kim DY, Jeon M. Data fusion of radar and image measurements for multi-object tracking via Kalman filtering. Inform Sci. 2014;27(6):43–9.MathSciNet
8.
go back to reference Wang Q. An adaptive fusion algorithm based on ANFIS for radar/infrared system. Expert Syst Appl. 2009;36(3):111–20. Wang Q. An adaptive fusion algorithm based on ANFIS for radar/infrared system. Expert Syst Appl. 2009;36(3):111–20.
Metadata
Title
A Novel In-flight Alignment Algorithm for Airborne Strapdown INS with Assistant of Doppler Radar
Authors
Shuang Pan
Xu Han
Nie Yongfang
Copyright Year
2015
DOI
https://doi.org/10.1007/978-3-319-13707-0_117