The use of an aircraft test stand for VTOL handling qualities studies

The VTOL flight tests stand for testing control concepts on the X-14B VSS aircraft in hover, is described. This stand permits realistic and safe piloted evaluation and checkout of various control systems and of parameter variations within each system to determine acceptability to the pilot. Pilots c...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Pauli, F. A., Corliss, L. D., Selan, S. D., Gerdes, R. M., Gossett, T. D.
Format: Report
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator Pauli, F. A.
Corliss, L. D.
Selan, S. D.
Gerdes, R. M.
Gossett, T. D.
description The VTOL flight tests stand for testing control concepts on the X-14B VSS aircraft in hover, is described. This stand permits realistic and safe piloted evaluation and checkout of various control systems and of parameter variations within each system to determine acceptability to the pilot. Pilots can use it as a practical training tool to practice procedures and flying techniques and become familiar with the aircraft characteristics. Some examples of test experience are given. The test stand allows the X14B to maneuver in hover from centered position + or - 9.7 deg in roll and + or - 9.3 deg in pitch, about + or - 6 deg in yaw, and + or - 15 cm in vertical translation. The unique vertical free flight freedom enables study of liftoffs and landings with power conditions duplicated. The response on the stand agrees well with that measured in free hovering flight, and pilot comments confirm this.
format Report
fullrecord <record><control><sourceid>nasa_CYI</sourceid><recordid>TN_cdi_nasa_ntrs_19740020624</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>19740020624</sourcerecordid><originalsourceid>FETCH-nasa_ntrs_197400206243</originalsourceid><addsrcrecordid>eNrjZHANyUhVKC1OVchPU0jMU0jMLEouSkwrUShJLS5RKC5JzEtRSMsvUggL8fdRyADycjLz0hUKSxNzMksyU4uBKkpTgDQPA2taYk5xKi-U5maQcXMNcfbQzUssTozPKykqjje0NDcxMDAyMDMyMSYgDQBqDS5b</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>The use of an aircraft test stand for VTOL handling qualities studies</title><source>NASA Technical Reports Server</source><creator>Pauli, F. A. ; Corliss, L. D. ; Selan, S. D. ; Gerdes, R. M. ; Gossett, T. D.</creator><creatorcontrib>Pauli, F. A. ; Corliss, L. D. ; Selan, S. D. ; Gerdes, R. M. ; Gossett, T. D.</creatorcontrib><description>The VTOL flight tests stand for testing control concepts on the X-14B VSS aircraft in hover, is described. This stand permits realistic and safe piloted evaluation and checkout of various control systems and of parameter variations within each system to determine acceptability to the pilot. Pilots can use it as a practical training tool to practice procedures and flying techniques and become familiar with the aircraft characteristics. Some examples of test experience are given. The test stand allows the X14B to maneuver in hover from centered position + or - 9.7 deg in roll and + or - 9.3 deg in pitch, about + or - 6 deg in yaw, and + or - 15 cm in vertical translation. The unique vertical free flight freedom enables study of liftoffs and landings with power conditions duplicated. The response on the stand agrees well with that measured in free hovering flight, and pilot comments confirm this.</description><language>eng</language><publisher>Legacy CDMS</publisher><subject>Facilities, Research, And Support</subject><creationdate>1974</creationdate><rights>Copyright Determination: GOV_PUBLIC_USE_PERMITTED</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>776,796</link.rule.ids><linktorsrc>$$Uhttps://ntrs.nasa.gov/citations/19740020624$$EView_record_in_NASA$$FView_record_in_$$GNASA$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Pauli, F. A.</creatorcontrib><creatorcontrib>Corliss, L. D.</creatorcontrib><creatorcontrib>Selan, S. D.</creatorcontrib><creatorcontrib>Gerdes, R. M.</creatorcontrib><creatorcontrib>Gossett, T. D.</creatorcontrib><title>The use of an aircraft test stand for VTOL handling qualities studies</title><description>The VTOL flight tests stand for testing control concepts on the X-14B VSS aircraft in hover, is described. This stand permits realistic and safe piloted evaluation and checkout of various control systems and of parameter variations within each system to determine acceptability to the pilot. Pilots can use it as a practical training tool to practice procedures and flying techniques and become familiar with the aircraft characteristics. Some examples of test experience are given. The test stand allows the X14B to maneuver in hover from centered position + or - 9.7 deg in roll and + or - 9.3 deg in pitch, about + or - 6 deg in yaw, and + or - 15 cm in vertical translation. The unique vertical free flight freedom enables study of liftoffs and landings with power conditions duplicated. The response on the stand agrees well with that measured in free hovering flight, and pilot comments confirm this.</description><subject>Facilities, Research, And Support</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1974</creationdate><recordtype>report</recordtype><sourceid>CYI</sourceid><recordid>eNrjZHANyUhVKC1OVchPU0jMU0jMLEouSkwrUShJLS5RKC5JzEtRSMsvUggL8fdRyADycjLz0hUKSxNzMksyU4uBKkpTgDQPA2taYk5xKi-U5maQcXMNcfbQzUssTozPKykqjje0NDcxMDAyMDMyMSYgDQBqDS5b</recordid><startdate>19740601</startdate><enddate>19740601</enddate><creator>Pauli, F. A.</creator><creator>Corliss, L. D.</creator><creator>Selan, S. D.</creator><creator>Gerdes, R. M.</creator><creator>Gossett, T. D.</creator><scope>CYE</scope><scope>CYI</scope></search><sort><creationdate>19740601</creationdate><title>The use of an aircraft test stand for VTOL handling qualities studies</title><author>Pauli, F. A. ; Corliss, L. D. ; Selan, S. D. ; Gerdes, R. M. ; Gossett, T. D.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-nasa_ntrs_197400206243</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1974</creationdate><topic>Facilities, Research, And Support</topic><toplevel>online_resources</toplevel><creatorcontrib>Pauli, F. A.</creatorcontrib><creatorcontrib>Corliss, L. D.</creatorcontrib><creatorcontrib>Selan, S. D.</creatorcontrib><creatorcontrib>Gerdes, R. M.</creatorcontrib><creatorcontrib>Gossett, T. D.</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Pauli, F. A.</au><au>Corliss, L. D.</au><au>Selan, S. D.</au><au>Gerdes, R. M.</au><au>Gossett, T. D.</au><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>The use of an aircraft test stand for VTOL handling qualities studies</btitle><date>1974-06-01</date><risdate>1974</risdate><abstract>The VTOL flight tests stand for testing control concepts on the X-14B VSS aircraft in hover, is described. This stand permits realistic and safe piloted evaluation and checkout of various control systems and of parameter variations within each system to determine acceptability to the pilot. Pilots can use it as a practical training tool to practice procedures and flying techniques and become familiar with the aircraft characteristics. Some examples of test experience are given. The test stand allows the X14B to maneuver in hover from centered position + or - 9.7 deg in roll and + or - 9.3 deg in pitch, about + or - 6 deg in yaw, and + or - 15 cm in vertical translation. The unique vertical free flight freedom enables study of liftoffs and landings with power conditions duplicated. The response on the stand agrees well with that measured in free hovering flight, and pilot comments confirm this.</abstract><cop>Legacy CDMS</cop><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_nasa_ntrs_19740020624
source NASA Technical Reports Server
subjects Facilities, Research, And Support
title The use of an aircraft test stand for VTOL handling qualities studies
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-16T07%3A36%3A13IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-nasa_CYI&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=The%20use%20of%20an%20aircraft%20test%20stand%20for%20VTOL%20handling%20qualities%20studies&rft.au=Pauli,%20F.%20A.&rft.date=1974-06-01&rft_id=info:doi/&rft_dat=%3Cnasa_CYI%3E19740020624%3C/nasa_CYI%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true