Method and device for the optimised management of the vertical path of an aircraft
The method involves comparing a predicted stabilization altitude with a setpoint stabilization altitude. An optimized vertical trajectory is provided as a function of determined current values of the parameters of an aircraft, and of difference between the predicted and setpoint stabilization altitu...
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| creator | LEFEBVRE, MICKAËL CONSTANS, FLORIAN |
| description | The method involves comparing a predicted stabilization altitude with a setpoint stabilization altitude. An optimized vertical trajectory is provided as a function of determined current values of the parameters of an aircraft, and of difference between the predicted and setpoint stabilization altitudes when the difference between the predicted stabilization altitude and the setpoint stabilization altitude is in an absolute value higher than a predefined altitude threshold. The optimized vertical trajectory is transmitted to guiding units (9) embedded on an on-board of an aircraft. An independent claim is also included for a device for optimizing management of a vertical path of an aircraft.
- Procédé et dispositif de gestion optimisée de la trajectoire verticale d'un aéronef
- Selon l'invention, le dispositif (1) comporte des moyens (21) pour prédire l'altitude de stabilisation à laquelle l'aéronef va atteindre une vitesse d'approche de consigne, des moyens (22) pour comparer l'altitude de stabilisation prédite à une altitude de stabilisation de consigne et des moyens (24) pour établir une trajectoire verticale optimisée lorsque la différence entre l'altitude de stabilisation prédite et l'altitude de stabilisation de consigne est supérieure à un seuil d'altitude prédéfini. |
| format | Patent |
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- Procédé et dispositif de gestion optimisée de la trajectoire verticale d'un aéronef
- Selon l'invention, le dispositif (1) comporte des moyens (21) pour prédire l'altitude de stabilisation à laquelle l'aéronef va atteindre une vitesse d'approche de consigne, des moyens (22) pour comparer l'altitude de stabilisation prédite à une altitude de stabilisation de consigne et des moyens (24) pour établir une trajectoire verticale optimisée lorsque la différence entre l'altitude de stabilisation prédite et l'altitude de stabilisation de consigne est supérieure à un seuil d'altitude prédéfini.</description><language>eng ; fre ; ger</language><subject>CONTROLLING ; PHYSICS ; REGULATING ; SIGNALLING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TRAFFIC CONTROL SYSTEMS</subject><creationdate>2013</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=20130130&DB=EPODOC&CC=EP&NR=2551836A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130130&DB=EPODOC&CC=EP&NR=2551836A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LEFEBVRE, MICKAËL</creatorcontrib><creatorcontrib>CONSTANS, FLORIAN</creatorcontrib><title>Method and device for the optimised management of the vertical path of an aircraft</title><description>The method involves comparing a predicted stabilization altitude with a setpoint stabilization altitude. An optimized vertical trajectory is provided as a function of determined current values of the parameters of an aircraft, and of difference between the predicted and setpoint stabilization altitudes when the difference between the predicted stabilization altitude and the setpoint stabilization altitude is in an absolute value higher than a predefined altitude threshold. The optimized vertical trajectory is transmitted to guiding units (9) embedded on an on-board of an aircraft. An independent claim is also included for a device for optimizing management of a vertical path of an aircraft.
- Procédé et dispositif de gestion optimisée de la trajectoire verticale d'un aéronef
- Selon l'invention, le dispositif (1) comporte des moyens (21) pour prédire l'altitude de stabilisation à laquelle l'aéronef va atteindre une vitesse d'approche de consigne, des moyens (22) pour comparer l'altitude de stabilisation prédite à une altitude de stabilisation de consigne et des moyens (24) pour établir une trajectoire verticale optimisée lorsque la différence entre l'altitude de stabilisation prédite et l'altitude de stabilisation de consigne est supérieure à un seuil d'altitude prédéfini.</description><subject>CONTROLLING</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SIGNALLING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TRAFFIC CONTROL SYSTEMS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNik0KwjAUBrNxIdU7vAu4qKXiVkqlG0HEfXkkX0yg-SF59PyieABXAzOzVY8bxCVDHA0ZrF6DbCokDpSy-OArDAWO_EJAFEr221YU8ZoXyizuIzkS-6ILW9mpjeWlYv9jo-g6PofpgJxm1MwaETKP92Pft-fudGm7P5Y3U6c3AQ</recordid><startdate>20130130</startdate><enddate>20130130</enddate><creator>LEFEBVRE, MICKAËL</creator><creator>CONSTANS, FLORIAN</creator><scope>EVB</scope></search><sort><creationdate>20130130</creationdate><title>Method and device for the optimised management of the vertical path of an aircraft</title><author>LEFEBVRE, MICKAËL ; CONSTANS, FLORIAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2551836A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2013</creationdate><topic>CONTROLLING</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SIGNALLING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TRAFFIC CONTROL SYSTEMS</topic><toplevel>online_resources</toplevel><creatorcontrib>LEFEBVRE, MICKAËL</creatorcontrib><creatorcontrib>CONSTANS, FLORIAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEFEBVRE, MICKAËL</au><au>CONSTANS, FLORIAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Method and device for the optimised management of the vertical path of an aircraft</title><date>2013-01-30</date><risdate>2013</risdate><abstract>The method involves comparing a predicted stabilization altitude with a setpoint stabilization altitude. An optimized vertical trajectory is provided as a function of determined current values of the parameters of an aircraft, and of difference between the predicted and setpoint stabilization altitudes when the difference between the predicted stabilization altitude and the setpoint stabilization altitude is in an absolute value higher than a predefined altitude threshold. The optimized vertical trajectory is transmitted to guiding units (9) embedded on an on-board of an aircraft. An independent claim is also included for a device for optimizing management of a vertical path of an aircraft.
- Procédé et dispositif de gestion optimisée de la trajectoire verticale d'un aéronef
- Selon l'invention, le dispositif (1) comporte des moyens (21) pour prédire l'altitude de stabilisation à laquelle l'aéronef va atteindre une vitesse d'approche de consigne, des moyens (22) pour comparer l'altitude de stabilisation prédite à une altitude de stabilisation de consigne et des moyens (24) pour établir une trajectoire verticale optimisée lorsque la différence entre l'altitude de stabilisation prédite et l'altitude de stabilisation de consigne est supérieure à un seuil d'altitude prédéfini.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | CONTROLLING PHYSICS REGULATING SIGNALLING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRAFFIC CONTROL SYSTEMS |
| title | Method and device for the optimised management of the vertical path of an aircraft |
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