A new boresighting method of the aircraft gun using a laser tracker. Issue 3 (15th June 2015)

• Record Type: Journal Article
• Authors: Wang, Qing; Huang, Peng; Li, Jiangxiong; Ke, Yinglin
• Is Part Of: Sensor review. Volume 35:Issue 3(2015)
• Page Start: 251
• Page End: 262
• Publication Date: 2015-06-15
• Subjects: Assembly -- Positioning -- Design for assembly -- Lasers -- Metrology; Sensor systems -- Periodicals; Detectors -- Industrial applications -- Periodicals; Engineering instruments -- Periodicals; 681.2
• DOI: 10.1108/SR-11-2014-740
• Languages: English
• ISSNs: 0260-2288

Abstract

Abstract : Purpose: – The purpose of this paper is to propose an innovative method to extend the operating range of the laser tracking system and improve the accuracy and automation of boresighting by designing a measurement instrument. Boresighting is a process that aligns the direction of special equipment with the aircraft reference axis. Sometimes the accurate measurement and adjustment of the equipment and the aircraft are hard to achieve. Design/methodology/approach: – The aircraft is moved by an automatic adjustment system which consists of three numerical control positioners. For obtaining the position of the bore axis, an instrument with two measurement points is designed. Based on the multivariate normal distribution hypothesis, an uncertainty evaluation method for the aiming points is introduced. The accuracy of the measurement point is described by an uncertainty ellipsoid. A compensation and calibration method is proposed to decrease the effect of manufacturing error and deflection error by the finite element analysis. Findings: – The experimental results of the boresighting measurement prove that the proposed method is effective and reliable in digital assembly. The measurement accuracy of the angle between the bore axis and the reference axis is about ±0.004°. In addition, the measurement result is mainly influenced by the position error of the instrument. Originality/value: – The results of this study will provide a new way to obtain and control the installation deviation of part in aircraft digital assembly and will help to improve the precision and efficiency. This measurement method can be applied to obtain the axis of a deep blind hole.