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Stable Algorithm For Estimating Airdata From Flush Surface Pressure MeasurementsAn airdata estimation and evaluation system and method, including a stable algorithm for estimating airdata from nonintrusive surface pressure measurements. The airdata estimation and evaluation system is preferably implemented in a flush airdata sensing (FADS) system. The system and method of the present invention take a flow model equation and transform it into a triples formulation equation. The triples formulation equation eliminates the pressure related states from the flow model equation by strategically taking the differences of three surface pressures, known as triples. This triples formulation equation is then used to accurately estimate and compute vital airdata from nonintrusive surface pressure measurements.
Document ID
20010095542
Acquisition Source
Armstrong Flight Research Center
Document Type
Other - Patent
Authors
Whitmore, Stephen, A.
(NASA Dryden Flight Research Center Edwards, CA United States)
Cobleigh, Brent R.
(NASA Dryden Flight Research Center Edwards, CA United States)
Haering, Edward A., Jr.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 7, 2013
Publication Date
June 26, 2001
Subject Category
Numerical Analysis
Report/Patent Number
Patent Number: NASA-Case-DRC-98022
Patent Number: US-Patent-6,253,166
Patent Application Number: US-Patent-Appl-SN-173608
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-DRC-98022|US-Patent-6,253,166
Patent Application
US-Patent-Appl-SN-173608
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