NACA-TR-1204

Application of several methods for determining transfer functions and frequency response of aircraft from flight data

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:37:58Z
date available	2017-09-04T15:37:58Z
date copyright	01/01/1954
date issued	1954
identifier other	OWRXYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/39967
description abstract	In the process of analyzing the longitudinal frequency-response characteristics of aircraft, information on some of the methods of analysis has been obtained by the Langley Aeronautical Laboratory of the National Advisory Committee for Aeronautics. In the investigation of these methods, the practical applications and limitations were stressed. In general, the methods considered may be classed as: (1) analysis of sinusoidal response, (2) analysis of transient response as to harmonic content through determination of the Fourier integral by manual or machine methods, and (3) analysis of the transient through the use of least-squares solutions of the coefficients of an assumed equation for either the transient time response or frequency response (sometimes referred to as curve-fitting methods). (author)
language	English
title	NACA-TR-1204	num
title	Application of several methods for determining transfer functions and frequency response of aircraft from flight data	en
type	standard
page	27
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1954
contenttype	fulltext