NASA NTRS · 20160004234
In-Flight Pitot-Static Calibration
Abstract
A GPS-based pitot-static calibration system uses global output-error optimization. High data rate measurements of static and total pressure, ambient air conditions, and GPS-based ground speed measurements are used to compute pitot-static pressure errors over a range of airspeed. System identification methods rapidly compute optimal pressure error models with defined confidence intervals.
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Foster, John V., Cunningham, Kevin. 2016-03-15. In-Flight Pitot-Static Calibration. https://ntrs.nasa.gov/citations/20160004234
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