Meteorological UAV Pitot-static tube wind error source and sensitivity analysis

In this paper analysis the error of meteorological UAV Pitot-static tube wind model, meteorological UAV source of error in measuring the wind model is divided into: airspeed error, ground speed error, structural error, motion state error and angle error of five parts, using error analysis and simula...

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Hauptverfasser: Yanjie Wang, Shudao Zhou, Hao Li, Guotao Zhu, Kejing Wei
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Shudao Zhou
Hao Li
Guotao Zhu
Kejing Wei
description In this paper analysis the error of meteorological UAV Pitot-static tube wind model, meteorological UAV source of error in measuring the wind model is divided into: airspeed error, ground speed error, structural error, motion state error and angle error of five parts, using error analysis and simulation to research the sensitivity of each error, to improve a good basis for the accuracy of meteorological UAV Pitot-static tube model.
doi_str_mv 10.1109/RSETE.2011.5964529
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subjects Aircraft navigation
Analytical models
Atmospheric measurements
Atmospheric modeling
Electron tubes
error analysis
error sources
Global Positioning System
Measurement uncertainty
meteorological UAV
pitot-static tube
simulation
wind model
title Meteorological UAV Pitot-static tube wind error source and sensitivity analysis
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