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.
Meteorological UAV Pitot-static tube wind error source and sensitivity analysis
01.06.2011
793369 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Further investigation of pitot-static tube
Engineering Index Backfile | 1935
|Pitot static tube factor at low Reynolds numbers
TIBKAT | 1932
|