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

Author

Wang, Yanjie ; Zhou, Shudao ; Li, Hao ; Zhu, Guotao ; Wei, Kejing

Author_Institution

Inst. of Meteorol., PLA Univ. of Sci. & Tech., Nanjing, China

fYear

2011

fDate

24-26 June 2011

Firstpage

1341

Lastpage

1344

Abstract

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.

Keywords

error analysis; meteorological instruments; remotely operated vehicles; sensitivity analysis; velocity measurement; wind; airspeed error; angle error; ground speed error; meteorological UAV; motion state error; pitot-static tube model; sensitivity analysis; structural error; wind error source; Aircraft navigation; Analytical models; Atmospheric measurements; Atmospheric modeling; Electron tubes; Global Positioning System; Measurement uncertainty; error analysis; error sources; meteorological UAV; pitot-static tube; simulation; wind model;

fLanguage

English

Publisher

ieee

Conference_Titel

Remote Sensing, Environment and Transportation Engineering (RSETE), 2011 International Conference on

Conference_Location

Nanjing

Print_ISBN

978-1-4244-9172-8

Type

conf

DOI

10.1109/RSETE.2011.5964529

Filename

5964529