OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET
Systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes the amount of payload that can be carried by an airplane. This is accomplished by determining an optimum initial pitch angle at rotation during takeoff which is ass...
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creator | KIM, Geun Il ROHR, Timothy C FREGNANI, Jose A |
description | Systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes the amount of payload that can be carried by an airplane. This is accomplished by determining an optimum initial pitch angle at rotation during takeoff which is associated with an optimum ratio of the takeoff safety speed to the stall speed that satisfies a specific set of climb/obstacle constraints. Targeting this optimum initial pitch angle allows the maximum takeoff gross weight that corresponds to the optimum takeoff safety speed/stall speed ratio to be selected. |
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This is accomplished by determining an optimum initial pitch angle at rotation during takeoff which is associated with an optimum ratio of the takeoff safety speed to the stall speed that satisfies a specific set of climb/obstacle constraints. Targeting this optimum initial pitch angle allows the maximum takeoff gross weight that corresponds to the optimum takeoff safety speed/stall speed ratio to be selected.</description><language>eng ; fre ; ger</language><subject>CONTROLLING ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><creationdate>2022</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220406&DB=EPODOC&CC=EP&NR=3528080B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220406&DB=EPODOC&CC=EP&NR=3528080B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KIM, Geun Il</creatorcontrib><creatorcontrib>ROHR, Timothy C</creatorcontrib><creatorcontrib>FREGNANI, Jose A</creatorcontrib><title>OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET</title><description>Systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes the amount of payload that can be carried by an airplane. 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language | eng ; fre ; ger |
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subjects | CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES |
title | OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET |
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