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Journal of Projectiles, Rockets, Missiles and Guidance >

2010 , Vol. 30 >Issue 2: 29 - 31

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.02.077

MISSILES AND GUIDANCE TECHNOLOGY

A New Maneuver Manner of Airborne Missile Transfer Alignment

  • LI Peng ,
  • LI Li ,
  • LU Fugang
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  • No.203 Research Institute of China Ordnance Industries, Xi'an 710065, China

Received date: 2009-10-14

  Online published: 2025-05-28

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Abstract

In order to found a project which adapts to airborne missile transfer alignment, considering errors resulting from data transmission delay, a Kalman filter model of transfer alignment scheme with an advanced “velocity + attitude" information matehing method to compensate these errors was built. A new maneuver for the simulation was designed. The simulation results show that with the compensation, the performance of the transfer alignment is improved visibly. Compared with common project, the maneuver manner has some better characters which can be simply, easily realized, and it is fit for helicopter.

Key words： transfer alignment; maneuver manner; delay error compensation; “velocity + attitude"; Kalman filtering

Cite this article

LI Peng , LI Li , LU Fugang . A New Maneuver Manner of Airborne Missile Transfer Alignment[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(2) : 29 -31 . DOI: 10.15892/j.cnki.djzdxb.2010.02.077

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