FR3044086B1 - Procede et dispositif de calcul d'une trajectoire securisee depuis la position courante d'un aeronef jusqu'a un point d'attache - Google Patents

Procede et dispositif de calcul d'une trajectoire securisee depuis la position courante d'un aeronef jusqu'a un point d'attache Download PDF

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Publication number
FR3044086B1
FR3044086B1 FR1502454A FR1502454A FR3044086B1 FR 3044086 B1 FR3044086 B1 FR 3044086B1 FR 1502454 A FR1502454 A FR 1502454A FR 1502454 A FR1502454 A FR 1502454A FR 3044086 B1 FR3044086 B1 FR 3044086B1
Authority
FR
France
Prior art keywords
attachment
aircraft
point
current position
trajectory
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
Application number
FR1502454A
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English (en)
Other versions
FR3044086A1 (fr
Inventor
Marianne Gillet
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Helicopters SAS
Original Assignee
Airbus Helicopters SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Helicopters SAS filed Critical Airbus Helicopters SAS
Priority to FR1502454A priority Critical patent/FR3044086B1/fr
Priority to US15/358,161 priority patent/US10013887B2/en
Publication of FR3044086A1 publication Critical patent/FR3044086A1/fr
Application granted granted Critical
Publication of FR3044086B1 publication Critical patent/FR3044086B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/003—Flight plan management
    • G08G5/0034—Assembly of a flight plan
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/20—Instruments for performing navigational calculations
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073—Surveillance aids
    • G08G5/0091—Surveillance aids for monitoring atmospheric conditions

Abstract

La présente invention concerne un procédé de calcul d'une trajectoire sécurisée depuis la position courante (P1) d'un aéronef jusqu'à un point d'attache (P2) au dessus d'un terrain au cours duquel on détermine ladite position courante (P1) dudit aéronef, puis on définit ledit point d'attache (P2) et on définit au moins une trajectoire d'attache (14) reliant, de façon sécurisée au dessus dudit terrain, ladite position courante (P1) audit point d'attache (P2). Ladite trajectoire d'attache (14) peut être décomposée en plusieurs chemins (31-39), chaque chemin (31-39) étant situé à une altitude sécurisée supérieure au point le plus haut du terrain que survole ledit aéronef. En outre, la trajectoire d'attache (14) peut être une trajectoire de retour définie par des points de passage (S1-S8) de l'aéronef (10).
FR1502454A 2015-11-24 2015-11-24 Procede et dispositif de calcul d'une trajectoire securisee depuis la position courante d'un aeronef jusqu'a un point d'attache Active FR3044086B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1502454A FR3044086B1 (fr) 2015-11-24 2015-11-24 Procede et dispositif de calcul d'une trajectoire securisee depuis la position courante d'un aeronef jusqu'a un point d'attache
US15/358,161 US10013887B2 (en) 2015-11-24 2016-11-22 Method and a device for calculating a safe path from the current position of an aircraft to an attachment point

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1502454 2015-11-24
FR1502454A FR3044086B1 (fr) 2015-11-24 2015-11-24 Procede et dispositif de calcul d'une trajectoire securisee depuis la position courante d'un aeronef jusqu'a un point d'attache

Publications (2)

Publication Number Publication Date
FR3044086A1 FR3044086A1 (fr) 2017-05-26
FR3044086B1 true FR3044086B1 (fr) 2018-05-18

Family

ID=56084069

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1502454A Active FR3044086B1 (fr) 2015-11-24 2015-11-24 Procede et dispositif de calcul d'une trajectoire securisee depuis la position courante d'un aeronef jusqu'a un point d'attache

Country Status (2)

Country Link
US (1) US10013887B2 (fr)
FR (1) FR3044086B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3415868A3 (fr) * 2015-07-14 2018-12-26 The Boeing Company Procédé et système de production autonome de chemins latéraux les plus courts pour systèmes aériens sans pilote

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2847553B1 (fr) 2002-11-27 2004-12-31 Eurocopter France Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segment
FR2853978B1 (fr) 2003-04-16 2006-02-03 Eurocopter France Procede et dispositif de securisation du vol d'un aeronef en conditions de vol aux instruments hors infrastructures de vol aux instruments
FR2874553B1 (fr) 2004-08-25 2007-12-14 Bruno Francis Alfred Avanzi Dispositif d'elements rigides depliables en partie haute d'une cellule de vehicule de loisirs avec, l'utilisation des verins de toit pour la depose au sol de la cellule dans une version amovible
FR2928726B1 (fr) * 2008-03-11 2013-05-17 Thales Sa Jonction d'une trajectoire civile et d'une trajectoire militaire
FR2945622B1 (fr) * 2009-05-15 2012-04-27 Thales Sa Procede de rejointe a court terme d'un plan de vol en guidage radar d'un aeronef
FR2947370B1 (fr) 2009-06-26 2011-11-25 Eurocopter France Procede d'aide au pilotage a basse altitude
US8633835B1 (en) * 2010-01-15 2014-01-21 The Boeing Company Display of climb capability for an aircraft based on potential states for the aircraft
US8886369B2 (en) * 2010-02-11 2014-11-11 The Boeing Company Vertical situation awareness system for aircraft
US8798814B1 (en) * 2011-01-27 2014-08-05 The Boeing Company Vertical situation awareness for rotorcraft
FR3017967B1 (fr) * 2014-02-21 2016-03-04 Thales Sa Procede et systeme de gestion de vol
CN104516354A (zh) 2014-12-25 2015-04-15 中国人民解放军总参谋部第六十研究所 一种无人直升机电力巡线智能返航路径控制方法

Also Published As

Publication number Publication date
US20170148330A1 (en) 2017-05-25
FR3044086A1 (fr) 2017-05-26
US10013887B2 (en) 2018-07-03

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