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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2014, Vol. 35 ›› Issue (9): 2568-2573.doi: 10.7527/S1000-6893.2014.0034

• Electronics and Control • Previous Articles     Next Articles

A Heading Correction Method for Airborne Navigation Equipment

WANG Quanxi1, HUANG Liang2, WANG Yang1   

  1. 1. Naval Armament Academy, Beijing 100161, China;
    2. College of Electronic Engineering, Naval University of Engineering, Wuhan 430033, China
  • Received:2013-11-18 Revised:2014-03-31 Online:2014-09-25 Published:2014-04-16

Abstract:

The heading correction problem of the small and medium-sized unmanned aerial vehicle (UAV) navigation equipment is discussed in this paper. To correct the heading data output from the UAV's magnetometer, this paper introduces a new method called "looking-back", which can obtain the heading angular misalignment data from airborne electro-optical pod and global positioning system (GPS). This method has significantly improved the accuracy of the target positioning of airborne electro-optical pod by correcting the UAV's heading data during the UAV flight test of verification. It can decrease the margin of error for the target azimuth from 2.5° to 0.5°, as well as to decrease the margin of error for the target distance from 3.0 km to 0.5 km. This test proves the validity and efficiency of the "looking-back" method for the correction for UAV heading.

Key words: unmanned aerial vehicles (UAV), magnetometer, heading correction, passive positioning, electro-optical pod

CLC Number: