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Airdata Calibration of a High-Performance Aircraft for Measuring Atmospheric Wind Profiles

Haering Jr., Edward A. (1990) Airdata Calibration of a High-Performance Aircraft for Measuring Atmospheric Wind Profiles. Technical Report NASA TM-101714, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

The research airdata system of an instrumented F-104 aircraft has been calibrated to measure winds aloft in support of the space shuttle wind measurement investigation at the National Aeronautics and Space Administration Ames Research Center Dryden Flight Research Facility. For this investigation, wind measurement accuracies comparable to those obtained from Jimsphere balloons were desired. This required an airdata calibration more accurate than needed for most aircraft research programs. The F-104 aircraft was equipped with a research pitot-static noseboom with integral angle-of-attack and flank angle-of-attack vanes and a ring-laser-gyro inertial reference unit. Tower fly-bys and radar acceleration-decelerations were used to calibrate Mach number and total temperature. Angle of attack and angle of sideslip were calibrated with a trajectory reconstruction technique using a multiple-state linear Kalman filter. The F-104 aircraft and instrumentation configuration, flight test maneuvers, data corrections, calibration techniques, and resulting calibrations and data repeatability are presented. Recommendations for future airdata systems on aircraft used to measure winds aloft are also given.

EPrint Type:NASA Technical Memorandum
Keywords:Airdata calibration, Trajectory reconstruction, Wind measurement
Subjects:(01 - 09) Aeronautics: (05) Aircraft Design, Testing And Performance
Aircraft/Project: Space Shuttle Orbiter
Aircraft/Project: F-104
ID Code:350
Deposited On:26 August 2004
Additional Information:27 pages. Prepared as AIAA 90-0320 for presentation at AIAA 28th Aerospace Sciences Meeting, Reno, Nevada, January 8–11, 1990.
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Last Modified: September 14, 2004
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