Test flight planning method for verifying maximum endurance index of piston power unmanned aerial vehicle

The invention discloses a test flight planning method for verifying the maximum endurance index of a piston power unmanned aerial vehicle, and the method comprises the steps: calculating the theoretical fuel consumption of the flight endurance of a test flight plan according to the maximum refueling...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	LUO LIHONG, LI JINJIE, ZHU JUN, GUO KAIQI, SHAO JINYI, CHENG JIEYUAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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	LUO LIHONG LI JINJIE ZHU JUN GUO KAIQI SHAO JINYI CHENG JIEYUAN
description	The invention discloses a test flight planning method for verifying the maximum endurance index of a piston power unmanned aerial vehicle, and the method comprises the steps: calculating the theoretical fuel consumption of the flight endurance of a test flight plan according to the maximum refueling amount of the unmanned aerial vehicle, the backup fuel amount, the maximum endurance index of the unmanned aerial vehicle, and the flight endurance of the test flight plan; calculating a take-off refueling amount according to the maximum refueling amount of the unmanned aerial vehicle, the backup fuel amount and the theoretical fuel consumption of the flight time of the test flight plan; according to the takeoff refueling amount and the in-vehicle fuel amount released after the unmanned aerial vehicle lands, the oil consumption of actual flight of the unmanned aerial vehicle is obtained; and according to the oil consumption of the actual flight of the unmanned aerial vehicle and the theoretical oil consumption of
format	Patent
fullrecord	<record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN116594430A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN116594430A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN116594430A3</originalsourceid><addsrcrecordid>eNqNjEEKwjAQRbtxIeodxgMIllbBpRTFlavuS2h-7EAyCUmq9fYW8QCuHnzef8uCW6RMxvJjyBSsEmF5kEMevCbjIz0R2by_o5rYjY4geoxKehCLxkTeUOCUvVDwL0Qaxc0ZaFLzVdm5MHBvsS4WRtmEzY-rYnu9tM1th-A7pKB6CHLX3MvyeDjVdbU_V_84H48CQTA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Test flight planning method for verifying maximum endurance index of piston power unmanned aerial vehicle</title><source>esp@cenet</source><creator>LUO LIHONG ; LI JINJIE ; ZHU JUN ; GUO KAIQI ; SHAO JINYI ; CHENG JIEYUAN</creator><creatorcontrib>LUO LIHONG ; LI JINJIE ; ZHU JUN ; GUO KAIQI ; SHAO JINYI ; CHENG JIEYUAN</creatorcontrib><description>The invention discloses a test flight planning method for verifying the maximum endurance index of a piston power unmanned aerial vehicle, and the method comprises the steps: calculating the theoretical fuel consumption of the flight endurance of a test flight plan according to the maximum refueling amount of the unmanned aerial vehicle, the backup fuel amount, the maximum endurance index of the unmanned aerial vehicle, and the flight endurance of the test flight plan; calculating a take-off refueling amount according to the maximum refueling amount of the unmanned aerial vehicle, the backup fuel amount and the theoretical fuel consumption of the flight time of the test flight plan; according to the takeoff refueling amount and the in-vehicle fuel amount released after the unmanned aerial vehicle lands, the oil consumption of actual flight of the unmanned aerial vehicle is obtained; and according to the oil consumption of the actual flight of the unmanned aerial vehicle and the theoretical oil consumption of</description><language>chi ; eng</language><subject>CONTROLLING ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><creationdate>2023</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=20230815&DB=EPODOC&CC=CN&NR=116594430A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230815&DB=EPODOC&CC=CN&NR=116594430A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LUO LIHONG</creatorcontrib><creatorcontrib>LI JINJIE</creatorcontrib><creatorcontrib>ZHU JUN</creatorcontrib><creatorcontrib>GUO KAIQI</creatorcontrib><creatorcontrib>SHAO JINYI</creatorcontrib><creatorcontrib>CHENG JIEYUAN</creatorcontrib><title>Test flight planning method for verifying maximum endurance index of piston power unmanned aerial vehicle</title><description>The invention discloses a test flight planning method for verifying the maximum endurance index of a piston power unmanned aerial vehicle, and the method comprises the steps: calculating the theoretical fuel consumption of the flight endurance of a test flight plan according to the maximum refueling amount of the unmanned aerial vehicle, the backup fuel amount, the maximum endurance index of the unmanned aerial vehicle, and the flight endurance of the test flight plan; calculating a take-off refueling amount according to the maximum refueling amount of the unmanned aerial vehicle, the backup fuel amount and the theoretical fuel consumption of the flight time of the test flight plan; according to the takeoff refueling amount and the in-vehicle fuel amount released after the unmanned aerial vehicle lands, the oil consumption of actual flight of the unmanned aerial vehicle is obtained; and according to the oil consumption of the actual flight of the unmanned aerial vehicle and the theoretical oil consumption of</description><subject>CONTROLLING</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjEEKwjAQRbtxIeodxgMIllbBpRTFlavuS2h-7EAyCUmq9fYW8QCuHnzef8uCW6RMxvJjyBSsEmF5kEMevCbjIz0R2by_o5rYjY4geoxKehCLxkTeUOCUvVDwL0Qaxc0ZaFLzVdm5MHBvsS4WRtmEzY-rYnu9tM1th-A7pKB6CHLX3MvyeDjVdbU_V_84H48CQTA</recordid><startdate>20230815</startdate><enddate>20230815</enddate><creator>LUO LIHONG</creator><creator>LI JINJIE</creator><creator>ZHU JUN</creator><creator>GUO KAIQI</creator><creator>SHAO JINYI</creator><creator>CHENG JIEYUAN</creator><scope>EVB</scope></search><sort><creationdate>20230815</creationdate><title>Test flight planning method for verifying maximum endurance index of piston power unmanned aerial vehicle</title><author>LUO LIHONG ; LI JINJIE ; ZHU JUN ; GUO KAIQI ; SHAO JINYI ; CHENG JIEYUAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116594430A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>CONTROLLING</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><toplevel>online_resources</toplevel><creatorcontrib>LUO LIHONG</creatorcontrib><creatorcontrib>LI JINJIE</creatorcontrib><creatorcontrib>ZHU JUN</creatorcontrib><creatorcontrib>GUO KAIQI</creatorcontrib><creatorcontrib>SHAO JINYI</creatorcontrib><creatorcontrib>CHENG JIEYUAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LUO LIHONG</au><au>LI JINJIE</au><au>ZHU JUN</au><au>GUO KAIQI</au><au>SHAO JINYI</au><au>CHENG JIEYUAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Test flight planning method for verifying maximum endurance index of piston power unmanned aerial vehicle</title><date>2023-08-15</date><risdate>2023</risdate><abstract>The invention discloses a test flight planning method for verifying the maximum endurance index of a piston power unmanned aerial vehicle, and the method comprises the steps: calculating the theoretical fuel consumption of the flight endurance of a test flight plan according to the maximum refueling amount of the unmanned aerial vehicle, the backup fuel amount, the maximum endurance index of the unmanned aerial vehicle, and the flight endurance of the test flight plan; calculating a take-off refueling amount according to the maximum refueling amount of the unmanned aerial vehicle, the backup fuel amount and the theoretical fuel consumption of the flight time of the test flight plan; according to the takeoff refueling amount and the in-vehicle fuel amount released after the unmanned aerial vehicle lands, the oil consumption of actual flight of the unmanned aerial vehicle is obtained; and according to the oil consumption of the actual flight of the unmanned aerial vehicle and the theoretical oil consumption of</abstract><oa>free_for_read</oa></addata></record>
fulltext	fulltext_linktorsrc
identifier
ispartof
issn
language	chi ; eng
recordid	cdi_epo_espacenet_CN116594430A
source	esp@cenet
subjects	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
title	Test flight planning method for verifying maximum endurance index of piston power unmanned aerial vehicle
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-29T18%3A22%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=LUO%20LIHONG&rft.date=2023-08-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN116594430A%3C/epo_EVB%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