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A Verification Method and Experimental Study of Data Transfer during Transfer Alignment on Moving Base

  • Yingchao Han
  • , Weixiao Meng*
  • , Baohua Song
  • *Corresponding author for this work
  • School of Electronics and Information Engineering, Harbin Institute of Technology
  • CAS - Institute of Electronics

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

Abstract

For mixed-guided airborne missiles, to ensure accurate handover from midcourse to terminal guidance, the carrier and missile shall be within a unified coordinate system during data transfer. To eliminate mounting precision errors and assess the missile-carrier alignment errors excited by different speeds, heights, attitudes, overloads, maneuvers and other conditions when elastic and torsional deformations are generated due to the aerodynamic force during the flight of the mounted missile, measurement methods are proposed in this paper. An engineeringly-feasible verification scheme for alignment error transfer relationships is also studied and developed through experiments, and the convergence speed and accuracy of the alignment algorithm are verified experimentally, proving that the scheme can be applied to evaluate transfer alignment on a moving base.

Original languageEnglish
Title of host publicationProceedings - 2022 6th International Conference on Imaging, Signal Processing and Communications, ICISPC 2022
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages139-142
Number of pages4
ISBN (Electronic)9781665454803
DOIs
StatePublished - 2022
Externally publishedYes
Event6th International Conference on Imaging, Signal Processing and Communications, ICISPC 2022 - Kumamoto, Japan
Duration: 22 Jul 202224 Jul 2022

Publication series

NameProceedings - 2022 6th International Conference on Imaging, Signal Processing and Communications, ICISPC 2022

Conference

Conference6th International Conference on Imaging, Signal Processing and Communications, ICISPC 2022
Country/TerritoryJapan
CityKumamoto
Period22/07/2224/07/22

Keywords

  • Airborne missile
  • alignment algorithm
  • data transfer
  • experimental verification

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