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Identification of Minimum Acceptable Characteristics for Manual STOL Flight Path Control. Volume3. Detailed Analyses and Tested Vehicle Characteristics
This report presents the detailed results and analysis procedures utilized to identify minimally acceptable flight path control characteristics of powered lift STOL airplanes. Deficiencies in flight path control are identified via closed loop analysis of describing function results obtained during t...
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creator | Hoh, Roger H Craig, Samuel J Ashkenas, Irving L |
description | This report presents the detailed results and analysis procedures utilized to identify minimally acceptable flight path control characteristics of powered lift STOL airplanes. Deficiencies in flight path control are identified via closed loop analysis of describing function results obtained during the simulation. Unacceptable characteristics for flare and landing are identified from correlations of pilot rating and commentary with key parameters obtained from closed loop pilot-vehicle analysis. A more concise summary of the overall program and the results is contained in Volume I.
See also Volume 1, ADA029249. |
format | report |
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See also Volume 1, ADA029249.</description><language>eng</language><subject>DYNAMIC RESPONSE ; FLIGHT CONTROL SYSTEMS ; FLIGHT PATHS ; FLIGHT SIMULATORS ; INSTRUMENT LANDINGS ; MANUAL OPERATION ; SHORT TAKEOFF AIRCRAFT ; STABILITY ; STABILIZATION SYSTEMS ; V/STOL</subject><creationdate>1976</creationdate><rights>Approved for public release; distribution is unlimited.</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/ADA029250$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Hoh, Roger H</creatorcontrib><creatorcontrib>Craig, Samuel J</creatorcontrib><creatorcontrib>Ashkenas, Irving L</creatorcontrib><creatorcontrib>SYSTEMS TECHNOLOGY INC HAWTHORNE CA</creatorcontrib><title>Identification of Minimum Acceptable Characteristics for Manual STOL Flight Path Control. Volume3. Detailed Analyses and Tested Vehicle Characteristics</title><description>This report presents the detailed results and analysis procedures utilized to identify minimally acceptable flight path control characteristics of powered lift STOL airplanes. Deficiencies in flight path control are identified via closed loop analysis of describing function results obtained during the simulation. Unacceptable characteristics for flare and landing are identified from correlations of pilot rating and commentary with key parameters obtained from closed loop pilot-vehicle analysis. A more concise summary of the overall program and the results is contained in Volume I.
See also Volume 1, ADA029249.</description><subject>DYNAMIC RESPONSE</subject><subject>FLIGHT CONTROL SYSTEMS</subject><subject>FLIGHT PATHS</subject><subject>FLIGHT SIMULATORS</subject><subject>INSTRUMENT LANDINGS</subject><subject>MANUAL OPERATION</subject><subject>SHORT TAKEOFF AIRCRAFT</subject><subject>STABILITY</subject><subject>STABILIZATION SYSTEMS</subject><subject>V/STOL</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1976</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFjTEKwkAQRdNYiHoDi7mAISRYWIbEoGBQMKSVcTNxBza7sjspPInXNYWdhdWD_z68efQ-dmSFe1Yo7Cy4Hmq2PIwD5ErRU_BuCAqNHpWQ5yCsAvTOQ412RAPX5nyCyvBDC1xQNBTOincmhtaZcaAshpIE2VAHuUXzChQAbQcNBZm2ljSr38QymvVoAq2-XETrat8Uh0032dt0sSS3vMyTdJduk-yP_gAA8k2n</recordid><startdate>197606</startdate><enddate>197606</enddate><creator>Hoh, Roger H</creator><creator>Craig, Samuel J</creator><creator>Ashkenas, Irving L</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197606</creationdate><title>Identification of Minimum Acceptable Characteristics for Manual STOL Flight Path Control. Volume3. Detailed Analyses and Tested Vehicle Characteristics</title><author>Hoh, Roger H ; Craig, Samuel J ; Ashkenas, Irving L</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA0292503</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1976</creationdate><topic>DYNAMIC RESPONSE</topic><topic>FLIGHT CONTROL SYSTEMS</topic><topic>FLIGHT PATHS</topic><topic>FLIGHT SIMULATORS</topic><topic>INSTRUMENT LANDINGS</topic><topic>MANUAL OPERATION</topic><topic>SHORT TAKEOFF AIRCRAFT</topic><topic>STABILITY</topic><topic>STABILIZATION SYSTEMS</topic><topic>V/STOL</topic><toplevel>online_resources</toplevel><creatorcontrib>Hoh, Roger H</creatorcontrib><creatorcontrib>Craig, Samuel J</creatorcontrib><creatorcontrib>Ashkenas, Irving L</creatorcontrib><creatorcontrib>SYSTEMS TECHNOLOGY INC HAWTHORNE CA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Hoh, Roger H</au><au>Craig, Samuel J</au><au>Ashkenas, Irving L</au><aucorp>SYSTEMS TECHNOLOGY INC HAWTHORNE CA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Identification of Minimum Acceptable Characteristics for Manual STOL Flight Path Control. Volume3. Detailed Analyses and Tested Vehicle Characteristics</btitle><date>1976-06</date><risdate>1976</risdate><abstract>This report presents the detailed results and analysis procedures utilized to identify minimally acceptable flight path control characteristics of powered lift STOL airplanes. Deficiencies in flight path control are identified via closed loop analysis of describing function results obtained during the simulation. Unacceptable characteristics for flare and landing are identified from correlations of pilot rating and commentary with key parameters obtained from closed loop pilot-vehicle analysis. A more concise summary of the overall program and the results is contained in Volume I.
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source | DTIC Technical Reports |
subjects | DYNAMIC RESPONSE FLIGHT CONTROL SYSTEMS FLIGHT PATHS FLIGHT SIMULATORS INSTRUMENT LANDINGS MANUAL OPERATION SHORT TAKEOFF AIRCRAFT STABILITY STABILIZATION SYSTEMS V/STOL |
title | Identification of Minimum Acceptable Characteristics for Manual STOL Flight Path Control. Volume3. Detailed Analyses and Tested Vehicle Characteristics |
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