Determining the Utility of Expanded Pitch Scale and Flightpath Angle as Display Parameters
The Research and Development Division of the USAF Instrument Flight Center (USAFIFC/RD) conducted a pilot factors evaluation to determine the utility of expanded pitch scale and flightpath angle (FPA) as display parameters. Ten subject pilots from the Instrument Flight Center participated in this ev...
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| creator | Barnette,James F Intano,Gabriel P |
| description | The Research and Development Division of the USAF Instrument Flight Center (USAFIFC/RD) conducted a pilot factors evaluation to determine the utility of expanded pitch scale and flightpath angle (FPA) as display parameters. Ten subject pilots from the Instrument Flight Center participated in this evaluation. Each subject pilot flew three sorties of approximately 1.3 hours duration in the RD NT-38 aircraft. Based on the responses of the subject pilots and observations of the project pilot, the Instrument Flight Center recommends expanded pitch be displayed on the ADI and FPA be displayed on the right side of the ADI. If a Head-Up Display (HUD) is available, then FPA should be displayed on the HUD. A further study should be conducted to determine the use of flightpath angle and expanded pitch in the high dynamic flight environment. (Author) |
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Ten subject pilots from the Instrument Flight Center participated in this evaluation. Each subject pilot flew three sorties of approximately 1.3 hours duration in the RD NT-38 aircraft. Based on the responses of the subject pilots and observations of the project pilot, the Instrument Flight Center recommends expanded pitch be displayed on the ADI and FPA be displayed on the right side of the ADI. If a Head-Up Display (HUD) is available, then FPA should be displayed on the HUD. A further study should be conducted to determine the use of flightpath angle and expanded pitch in the high dynamic flight environment. (Author)</description><language>eng</language><subject>ANGLES ; DISPLAY SYSTEMS ; Flight Control and Instrumentation ; FLIGHT INSTRUMENTS ; FLIGHT PATHS ; FLIGHT TESTING ; HEAD UP DISPLAYS ; HUMAN FACTORS ENGINEERING ; Human Factors Engineering & Man Machine System ; PITCH(INCLINATION) ; SCALING FACTOR</subject><creationdate>1976</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/ADA031990$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Barnette,James F</creatorcontrib><creatorcontrib>Intano,Gabriel P</creatorcontrib><creatorcontrib>INSTRUMENT FLIGHT CENTER RANDOLPH AFB TEX</creatorcontrib><title>Determining the Utility of Expanded Pitch Scale and Flightpath Angle as Display Parameters</title><description>The Research and Development Division of the USAF Instrument Flight Center (USAFIFC/RD) conducted a pilot factors evaluation to determine the utility of expanded pitch scale and flightpath angle (FPA) as display parameters. Ten subject pilots from the Instrument Flight Center participated in this evaluation. Each subject pilot flew three sorties of approximately 1.3 hours duration in the RD NT-38 aircraft. Based on the responses of the subject pilots and observations of the project pilot, the Instrument Flight Center recommends expanded pitch be displayed on the ADI and FPA be displayed on the right side of the ADI. If a Head-Up Display (HUD) is available, then FPA should be displayed on the HUD. A further study should be conducted to determine the use of flightpath angle and expanded pitch in the high dynamic flight environment. (Author)</description><subject>ANGLES</subject><subject>DISPLAY SYSTEMS</subject><subject>Flight Control and Instrumentation</subject><subject>FLIGHT INSTRUMENTS</subject><subject>FLIGHT PATHS</subject><subject>FLIGHT TESTING</subject><subject>HEAD UP DISPLAYS</subject><subject>HUMAN FACTORS ENGINEERING</subject><subject>Human Factors Engineering & Man Machine System</subject><subject>PITCH(INCLINATION)</subject><subject>SCALING FACTOR</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1976</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFjLEKwjAQQLM4iPoHDvcDQqVTx2BaHAvq4lKO5JocpDE0N9i_14K704P34G3V05DQPHHi5EECwUM4sizwGqF9Z0yOHPQsNsDNYiT4Gugi-yAZJYBOfpUFDJcccYEeZ5zWZ9mrzYix0OHHnTp27f1yPTlhOxThRDJoo6v63DRV_Sd_AHOaN1U</recordid><startdate>197610</startdate><enddate>197610</enddate><creator>Barnette,James F</creator><creator>Intano,Gabriel P</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>197610</creationdate><title>Determining the Utility of Expanded Pitch Scale and Flightpath Angle as Display Parameters</title><author>Barnette,James F ; Intano,Gabriel P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA0319903</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1976</creationdate><topic>ANGLES</topic><topic>DISPLAY SYSTEMS</topic><topic>Flight Control and Instrumentation</topic><topic>FLIGHT INSTRUMENTS</topic><topic>FLIGHT PATHS</topic><topic>FLIGHT TESTING</topic><topic>HEAD UP DISPLAYS</topic><topic>HUMAN FACTORS ENGINEERING</topic><topic>Human Factors Engineering & Man Machine System</topic><topic>PITCH(INCLINATION)</topic><topic>SCALING FACTOR</topic><toplevel>online_resources</toplevel><creatorcontrib>Barnette,James F</creatorcontrib><creatorcontrib>Intano,Gabriel P</creatorcontrib><creatorcontrib>INSTRUMENT FLIGHT CENTER RANDOLPH AFB TEX</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Barnette,James F</au><au>Intano,Gabriel P</au><aucorp>INSTRUMENT FLIGHT CENTER RANDOLPH AFB TEX</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Determining the Utility of Expanded Pitch Scale and Flightpath Angle as Display Parameters</btitle><date>1976-10</date><risdate>1976</risdate><abstract>The Research and Development Division of the USAF Instrument Flight Center (USAFIFC/RD) conducted a pilot factors evaluation to determine the utility of expanded pitch scale and flightpath angle (FPA) as display parameters. Ten subject pilots from the Instrument Flight Center participated in this evaluation. Each subject pilot flew three sorties of approximately 1.3 hours duration in the RD NT-38 aircraft. Based on the responses of the subject pilots and observations of the project pilot, the Instrument Flight Center recommends expanded pitch be displayed on the ADI and FPA be displayed on the right side of the ADI. If a Head-Up Display (HUD) is available, then FPA should be displayed on the HUD. A further study should be conducted to determine the use of flightpath angle and expanded pitch in the high dynamic flight environment. (Author)</abstract><oa>free_for_read</oa></addata></record> |
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| source | DTIC Technical Reports |
| subjects | ANGLES DISPLAY SYSTEMS Flight Control and Instrumentation FLIGHT INSTRUMENTS FLIGHT PATHS FLIGHT TESTING HEAD UP DISPLAYS HUMAN FACTORS ENGINEERING Human Factors Engineering & Man Machine System PITCH(INCLINATION) SCALING FACTOR |
| title | Determining the Utility of Expanded Pitch Scale and Flightpath Angle as Display Parameters |
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