FR3110020B1 - Method and electronic system for aiding the management of the flight of an aircraft with management of loop(s), associated computer program - Google Patents
Method and electronic system for aiding the management of the flight of an aircraft with management of loop(s), associated computer program Download PDFInfo
- Publication number
- FR3110020B1 FR3110020B1 FR2004436A FR2004436A FR3110020B1 FR 3110020 B1 FR3110020 B1 FR 3110020B1 FR 2004436 A FR2004436 A FR 2004436A FR 2004436 A FR2004436 A FR 2004436A FR 3110020 B1 FR3110020 B1 FR 3110020B1
- Authority
- FR
- France
- Prior art keywords
- management
- flight
- loop
- aircraft
- aiding
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
- G08G5/21—Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/30—Flight plan management
- G08G5/34—Flight plan management for flight plan modification
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/53—Navigation or guidance aids for cruising
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/54—Navigation or guidance aids for approach or landing
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/55—Navigation or guidance aids for a single aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/58—Navigation or guidance aids for emergency situations, e.g. hijacking or bird strikes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Traffic Control Systems (AREA)
- Navigation (AREA)
Abstract
Procédé et système électronique d’aide à la gestion du vol d’un aéronef avec gestion de boucle(s), programme d’ordinateur associé Ce procédé d’aide à la gestion du vol d’un aéronef est mis en œuvre par un système électronique d’aide à la gestion de vol et comprend les étapes suivantes : - l’acquisition (100) de premier et deuxième points caractéristiques d’une boucle à insérer dans un plan de vol de l’aéronef ; - le calcul (110) d’une trajectoire de boucle à partir des premier et deuxième points caractéristiques acquis, le premier point caractéristique formant un point de début de la trajectoire de boucle et le deuxième point caractéristique étant un point pour un retour vers le premier point caractéristique ; et - la génération (120) d’un plan de vol modifié à partir d’un plan de vol courant, le plan de vol modifié étant obtenu par insertion, dans le plan de vol courant et à partir du premier point caractéristique, de la trajectoire de boucle calculée. Figure pour l'abrégé : Figure 4Method and electronic system for aiding the management of the flight of an aircraft with management of loop(s), associated computer program This method for aiding the management of the flight of an aircraft is implemented by a system electronic flight management aid and comprises the following steps: - the acquisition (100) of first and second characteristic points of a loop to be inserted into a flight plan of the aircraft; - the calculation (110) of a loop trajectory from the first and second characteristic points acquired, the first characteristic point forming a start point of the loop trajectory and the second characteristic point being a point for a return to the first characteristic point; and - the generation (120) of a modified flight plan from a current flight plan, the modified flight plan being obtained by inserting, into the current flight plan and from the first characteristic point, the calculated loop trajectory. Figure for abstract: Figure 4
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2004436A FR3110020B1 (en) | 2020-05-05 | 2020-05-05 | Method and electronic system for aiding the management of the flight of an aircraft with management of loop(s), associated computer program |
EP21722496.3A EP4147218A1 (en) | 2020-05-05 | 2021-05-05 | Method and electronic system for aircraft flight management assistance with loop management and associated computer program |
PCT/EP2021/061795 WO2021224299A1 (en) | 2020-05-05 | 2021-05-05 | Method and electronic system for aircraft flight management assistance with loop management and associated computer program |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2004436A FR3110020B1 (en) | 2020-05-05 | 2020-05-05 | Method and electronic system for aiding the management of the flight of an aircraft with management of loop(s), associated computer program |
FR2004436 | 2020-05-05 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3110020A1 FR3110020A1 (en) | 2021-11-12 |
FR3110020B1 true FR3110020B1 (en) | 2023-03-03 |
Family
ID=72644304
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2004436A Active FR3110020B1 (en) | 2020-05-05 | 2020-05-05 | Method and electronic system for aiding the management of the flight of an aircraft with management of loop(s), associated computer program |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP4147218A1 (en) |
FR (1) | FR3110020B1 (en) |
WO (1) | WO2021224299A1 (en) |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2894368B1 (en) * | 2005-12-07 | 2008-01-25 | Thales Sa | DEVICE AND METHOD FOR AUTOMATED CONSTRUCTION OF EMERGENCY TRACK FOR AIRCRAFT |
FR2915824B1 (en) * | 2007-05-02 | 2009-06-05 | Thales Sa | METHOD OF OPTIMIZING THE OUTPUT OF AN AIRCRAFT IN A WAITING CIRCUIT |
US10692386B2 (en) * | 2018-09-28 | 2020-06-23 | Aviation Mobile Apps, LLC | Holding pattern determination |
-
2020
- 2020-05-05 FR FR2004436A patent/FR3110020B1/en active Active
-
2021
- 2021-05-05 EP EP21722496.3A patent/EP4147218A1/en active Pending
- 2021-05-05 WO PCT/EP2021/061795 patent/WO2021224299A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
FR3110020A1 (en) | 2021-11-12 |
WO2021224299A1 (en) | 2021-11-11 |
EP4147218A1 (en) | 2023-03-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20211112 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |