METHOD FOR DETERMINING A POSITION ERROR CORRECTION ON A STATIC PRESSURE MEASUREMENT AT AN AIRCRAFT
The invention provides a method for determining a position error correction on a static pressure measurement at an aircraft flying through a flow field by means of a Taylor expansion series. The method comprises determining the constants of such a Taylor expansion series by the successive steps of a...
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| creator | Dumoulin, Thomas Eugene Francois Jean Laban, Martin |
| description | The invention provides a method for determining a position error correction on a static pressure measurement at an aircraft flying through a flow field by means of a Taylor expansion series. The method comprises determining the constants of such a Taylor expansion series by the successive steps of an initial determination using computational fluid dynamics and a 3D scan of the aircraft, a validation of the results by low altitude flyby's at a ground station and an extrapolation of the results to altitude by performing flight tests at constant altitude and conditions of constant atmospheric pressure. |
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| subjects | GYROSCOPIC INSTRUMENTS INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING |
| title | METHOD FOR DETERMINING A POSITION ERROR CORRECTION ON A STATIC PRESSURE MEASUREMENT AT AN AIRCRAFT |
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