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- W2536294050 abstract "A technique for the identification of aircraft stability and control parameters fromflight test recordings made in either calm or turbulent air is presented. The maximumlikelihood output error method is used with a steady-state Kalman filter incorporatedto account for atmospheric turbulence. A modified Newton-Raphson search technique,enhanced by a line search, is employed for parameter identification. Separatealgorithms are developed for estimating the biases and noise levels in the observations.Some areas of practical problems in the application of such methods are stressed. Acomputer program for the identification of longitudinal stability derivatives isdescribed and the aircraft instrumentation required is exemplified by that in GnatXPSOS. The wind tunnel calibration of the flow-direction sensing nose probeassembly of Conrad yawmeters on this aircraft is detailed. The problems of handlingthe flight observations recorded are covered and some of the troubles experiencedwith the instruments are noted.The performance of the identification technique is investigated. The data required,the choices open to the analyst and the statistical information produced being highlighted.The identification of the process noise level, in this instance the turbulenceintensity, is addressed and it is found that the value specified for this level caninfluence the other parameters.The longitudinal stability and control derivatives obtained for Gnat XPSOS arepresented." @default.
- W2536294050 created "2016-10-28" @default.
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- W2536294050 date "1982-07-01" @default.
- W2536294050 modified "2023-09-27" @default.
- W2536294050 title "The identification of aircraft stability and control parameters in turbulence" @default.
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