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NASA-TP-1306

Determination of stability and control parameters of a light airplane from flight data using two estimation methods

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:20:43Z
date available2017-09-04T17:20:43Z
date copyright01/01/1979
date issued1979
identifier otherZQYKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/143903
description abstractTwo identification methods, the equation error method and the output error method, are used to estimate stability and control parameter values from flight data for a low-wing, single-engine, general aviation airplane. The estimated parameters from both methods are in very good agreement primarily because of sufficient accuracy of measured data. The estimated static parameters also agree with the results from steady flights. The effect of power different input forms are demonstrated. Examination of all results available gives the best values of estimated parameters and specifies their accuracies.
languageEnglish
titleNASA-TP-1306num
titleDetermination of stability and control parameters of a light airplane from flight data using two estimation methodsen
typestandard
page103
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1979
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsANALYSIS
subject keywordsCHARACTERISTICS
subject keywordsCONTROL
subject keywordsEQUATIONS
subject keywordsESTIMATES
subject keywordsFLIGHT
subject keywordsLEAST
subject keywordsLIGHT
subject keywordsLIKELIHOOD
subject keywordsMAXIMUM
subject keywordsMETHOD
subject keywordsMONITORING
subject keywordsMOTION
subject keywordsPARAMETERIZATION
subject keywordsREGRESSION
subject keywordsSQUARES
subject keywordsSTABILITY
subject keywordsSURFACES


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