Paper
12 March 2019 Errors analysis of laser relative navigation for fixed wing aircraft landing
Jingting Su, Yang Xie, Qi Zhou
Author Affiliations +
Proceedings Volume 11023, Fifth Symposium on Novel Optoelectronic Detection Technology and Application; 110230R (2019) https://doi.org/10.1117/12.2520494
Event: Fifth Symposium on Novel Optoelectronic Detection Technology and Application, 2018, Xi'an, China
Abstract
A high precision measuring device is required during the fixed-wing aircraft landing. In order to improve accuracy of laser scanning system, a scanning measurement model is established to carry out error analysis. The measurement error simulation is carried out for two cases without sea-wave disturbance and sea-wave disturbance, and the variation law of angle measurement error is obtained. The results show that the angle error becomes lager as the plane gets closer and closer to the landing point, and the error reaches the maximum when the plane landed. The wave disturbance will cause a small range of jitter in error curve, and the amplitude will increase slightly. The result provides a theoretical reference for the compensation correction of laser scanning measurement system.
© (2019) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Jingting Su, Yang Xie, and Qi Zhou "Errors analysis of laser relative navigation for fixed wing aircraft landing", Proc. SPIE 11023, Fifth Symposium on Novel Optoelectronic Detection Technology and Application, 110230R (12 March 2019); https://doi.org/10.1117/12.2520494
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Error analysis

Laser scanners

Distance measurement

Laser systems engineering

Computer simulations

Measurement devices

Motion models

Back to Top