Uncertainty methodology for in-flight thrust determinationA methodology is proposed for the evaluation of uncertainty in the in-flight determination of aircraft thrust, which provides error traceability to a national standards laboratory, and is independent of the procedure used to calculate or measure thrust in flight, thereby yielding a consistent means for the evaluation of measurement capabilities. Attention is given to the factors of measurement error, precision, bias, uncertainty, error estimation and classification, error propagation, ground testing, and the related problems of model bias error, model precision error, and the uncertainty limit.
Document ID
19840046665
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Adams, G. R. (USAF Wright-Patterson AFB, OH, United States)
Thompson, J. W., Jr. (Sverdrup Technology, Inc. Tullahoma, TN, United States)
Abernethy, R. B. (United Technologies Corp. Pratt and Whitney Group, East Hartford, CT, United States)
Biesiadny, T. (NASA Lewis Research Center Cleveland, OH, United States)
Havey, C. T. (Boeing Military Airplane Co. Wichita, KS, United States)
Steurer, J. W. (McDonnell Aircraft Co. St. Louis, MO, United States)
Ascough, J. C. (Royal Aircraft Establishment Farnborough, Hants., United Kingdom)
Williams, D. D. (Rolls-Royce, Ltd. London, United Kingdom)