Helicopter System Dynamics Identification
Methods are discussed which can be used to identify helicopter system dynamics. Stochastic and deterministic techniques are presented and the latter method is applied to flight test data. The stochastic technique is based on the Maximum Likelihood (ML) criterion and can be reduced to the determinist...
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creator | Fermelia, A |
description | Methods are discussed which can be used to identify helicopter system dynamics. Stochastic and deterministic techniques are presented and the latter method is applied to flight test data. The stochastic technique is based on the Maximum Likelihood (ML) criterion and can be reduced to the deterministic case. A computer program listing of the deterministic method is given. |
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The stochastic technique is based on the Maximum Likelihood (ML) criterion and can be reduced to the deterministic case. A computer program listing of the deterministic method is given.</description><language>eng</language><subject>Aerodynamics ; COMPUTER PROGRAMS ; COMPUTERIZED SIMULATION ; Deterministic methods ; FLIGHT ; Flight dynamics ; FLIGHT PATHS ; Helicopters ; MATRICES(MATHEMATICS) ; Military Aircraft Operations ; Navigation and Guidance ; PROBABILITY DENSITY FUNCTIONS ; TRANSFORMATIONS(MATHEMATICS)</subject><creationdate>1973</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA005216$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Fermelia, A</creatorcontrib><creatorcontrib>MISSOURI UNIV-ROLLA</creatorcontrib><title>Helicopter System Dynamics Identification</title><description>Methods are discussed which can be used to identify helicopter system dynamics. Stochastic and deterministic techniques are presented and the latter method is applied to flight test data. The stochastic technique is based on the Maximum Likelihood (ML) criterion and can be reduced to the deterministic case. A computer program listing of the deterministic method is given.</description><subject>Aerodynamics</subject><subject>COMPUTER PROGRAMS</subject><subject>COMPUTERIZED SIMULATION</subject><subject>Deterministic methods</subject><subject>FLIGHT</subject><subject>Flight dynamics</subject><subject>FLIGHT PATHS</subject><subject>Helicopters</subject><subject>MATRICES(MATHEMATICS)</subject><subject>Military Aircraft Operations</subject><subject>Navigation and Guidance</subject><subject>PROBABILITY DENSITY FUNCTIONS</subject><subject>TRANSFORMATIONS(MATHEMATICS)</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1973</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZND0SM3JTM4vKEktUgiuLC5JzVVwqcxLzM1MLlbwTEnNK8lMy0xOLMnMz-NhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji6OBgamRoZmxgSkAYLPJf4</recordid><startdate>197312</startdate><enddate>197312</enddate><creator>Fermelia, A</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197312</creationdate><title>Helicopter System Dynamics Identification</title><author>Fermelia, A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA0052163</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1973</creationdate><topic>Aerodynamics</topic><topic>COMPUTER PROGRAMS</topic><topic>COMPUTERIZED SIMULATION</topic><topic>Deterministic methods</topic><topic>FLIGHT</topic><topic>Flight dynamics</topic><topic>FLIGHT PATHS</topic><topic>Helicopters</topic><topic>MATRICES(MATHEMATICS)</topic><topic>Military Aircraft Operations</topic><topic>Navigation and Guidance</topic><topic>PROBABILITY DENSITY FUNCTIONS</topic><topic>TRANSFORMATIONS(MATHEMATICS)</topic><toplevel>online_resources</toplevel><creatorcontrib>Fermelia, A</creatorcontrib><creatorcontrib>MISSOURI UNIV-ROLLA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Fermelia, A</au><aucorp>MISSOURI UNIV-ROLLA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Helicopter System Dynamics Identification</btitle><date>1973-12</date><risdate>1973</risdate><abstract>Methods are discussed which can be used to identify helicopter system dynamics. Stochastic and deterministic techniques are presented and the latter method is applied to flight test data. The stochastic technique is based on the Maximum Likelihood (ML) criterion and can be reduced to the deterministic case. A computer program listing of the deterministic method is given.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng |
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source | DTIC Technical Reports |
subjects | Aerodynamics COMPUTER PROGRAMS COMPUTERIZED SIMULATION Deterministic methods FLIGHT Flight dynamics FLIGHT PATHS Helicopters MATRICES(MATHEMATICS) Military Aircraft Operations Navigation and Guidance PROBABILITY DENSITY FUNCTIONS TRANSFORMATIONS(MATHEMATICS) |
title | Helicopter System Dynamics Identification |
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