FR3018364B1 - Procede de determination d'une loi de guidage d'evitement d'obstacle par un aeronef, produit programme d'ordinateur, systeme electronique et aeronef associes - Google Patents

Procede de determination d'une loi de guidage d'evitement d'obstacle par un aeronef, produit programme d'ordinateur, systeme electronique et aeronef associes

Info

Publication number
FR3018364B1
FR3018364B1 FR1400537A FR1400537A FR3018364B1 FR 3018364 B1 FR3018364 B1 FR 3018364B1 FR 1400537 A FR1400537 A FR 1400537A FR 1400537 A FR1400537 A FR 1400537A FR 3018364 B1 FR3018364 B1 FR 3018364B1
Authority
FR
France
Prior art keywords
aircraft
obstacle
determining
computer program
program product
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
FR1400537A
Other languages
English (en)
Other versions
FR3018364A1 (fr
Inventor
Matthieu Claybrough
Francois Colonna
Marc Riedinger
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.)
Thales SA
Original Assignee
Thales SA
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 Thales SA filed Critical Thales SA
Priority to FR1400537A priority Critical patent/FR3018364B1/fr
Priority to CA2881545A priority patent/CA2881545C/fr
Priority to US14/625,739 priority patent/US9418564B2/en
Priority to BR102015004715A priority patent/BR102015004715A2/pt
Priority to CN201510095600.5A priority patent/CN104900092B/zh
Priority to RU2015107383A priority patent/RU2683718C2/ru
Publication of FR3018364A1 publication Critical patent/FR3018364A1/fr
Application granted granted Critical
Publication of FR3018364B1 publication Critical patent/FR3018364B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/04—Anti-collision systems
    • G08G5/045—Navigation or guidance aids, e.g. determination of anti-collision manoeuvers
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/04—Anti-collision systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • 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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/10—Complex mathematical operations
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Automation & Control Theory (AREA)
  • Mathematical Physics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Algebra (AREA)
  • Data Mining & Analysis (AREA)
  • Theoretical Computer Science (AREA)
  • Computational Mathematics (AREA)
  • Databases & Information Systems (AREA)
  • Software Systems (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Traffic Control Systems (AREA)
FR1400537A 2014-03-04 2014-03-04 Procede de determination d'une loi de guidage d'evitement d'obstacle par un aeronef, produit programme d'ordinateur, systeme electronique et aeronef associes Active FR3018364B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR1400537A FR3018364B1 (fr) 2014-03-04 2014-03-04 Procede de determination d'une loi de guidage d'evitement d'obstacle par un aeronef, produit programme d'ordinateur, systeme electronique et aeronef associes
CA2881545A CA2881545C (fr) 2014-03-04 2015-02-09 Methode permettant de determiner une loi d'orientation en vue de l'evitement d'un obstacle par un aeronef, produit de programme informatique associe, dispositif electronique et aeronef
US14/625,739 US9418564B2 (en) 2014-03-04 2015-02-19 Method for determining a guidance law for obstacle avoidance by an aircraft, related computer program product, electronic system and aircraft
BR102015004715A BR102015004715A2 (pt) 2014-03-04 2015-03-03 método para determinar uma lei de orientação de evasão, meio legível por computador, sistema de determinação eletrônica e aeronave
CN201510095600.5A CN104900092B (zh) 2014-03-04 2015-03-03 用于确定飞行器的回避导引律的方法、电子系统和飞行器
RU2015107383A RU2683718C2 (ru) 2014-03-04 2015-03-03 Способ определения закона наведения для уклонения от препятствия летательным аппаратом, электронная система и летательный аппарат

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1400537A FR3018364B1 (fr) 2014-03-04 2014-03-04 Procede de determination d'une loi de guidage d'evitement d'obstacle par un aeronef, produit programme d'ordinateur, systeme electronique et aeronef associes

Publications (2)

Publication Number Publication Date
FR3018364A1 FR3018364A1 (fr) 2015-09-11
FR3018364B1 true FR3018364B1 (fr) 2016-04-01

Family

ID=51225579

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1400537A Active FR3018364B1 (fr) 2014-03-04 2014-03-04 Procede de determination d'une loi de guidage d'evitement d'obstacle par un aeronef, produit programme d'ordinateur, systeme electronique et aeronef associes

Country Status (6)

Country Link
US (1) US9418564B2 (fr)
CN (1) CN104900092B (fr)
BR (1) BR102015004715A2 (fr)
CA (1) CA2881545C (fr)
FR (1) FR3018364B1 (fr)
RU (1) RU2683718C2 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10192453B2 (en) * 2016-07-13 2019-01-29 Honeywell International Inc. Aircraft traffic alert and collision avoidance system with autoflight system mode protection
US10885798B2 (en) * 2016-07-13 2021-01-05 Honeywell International Inc. Aircraft traffic alert and collision avoidance system with autoflight system mode protection
CN106200654A (zh) * 2016-09-28 2016-12-07 北京小米移动软件有限公司 无人机飞行速度的控制方法和装置
EP3671698A1 (fr) * 2018-12-19 2020-06-24 Honeywell International Inc. Alerte de la circulation d'aéronef et système d'évitement de collision avec protection en mode système de pilotage automatique
US11164471B1 (en) 2019-10-04 2021-11-02 The Boeing Company System for previewing vertical speed guidance following an air traffic conflict alert
CN113688463B (zh) * 2020-05-18 2024-01-23 中国航发商用航空发动机有限责任公司 导线碰撞角度范围筛选方法和装置、计算机可读存储介质
CN113220008B (zh) * 2021-05-21 2022-11-25 南京航空航天大学 多火星飞行器的协同动态路径规划方法
CN115059549B (zh) * 2022-06-16 2024-01-02 中国航发沈阳发动机研究所 一种防止大马赫数误操作油门杆的控制方法及系统

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0750238B1 (fr) * 1995-06-20 2000-03-01 Honeywell Inc. Système intégré d'anti-collision avec le sol
US6700482B2 (en) * 2000-09-29 2004-03-02 Honeywell International Inc. Alerting and notification system
US6873269B2 (en) * 2003-05-27 2005-03-29 Honeywell International Inc. Embedded free flight obstacle avoidance system
US20050113985A1 (en) * 2003-11-26 2005-05-26 Safe Flight Instrument Corporation Obstacle avoidance system for rotary wing aircraft
FR2876483B1 (fr) * 2004-10-08 2007-07-20 Airbus France Sas Procede et systeme d'evitement pour un aeronef
FR2893147B1 (fr) * 2005-11-10 2010-12-10 Thales Sa Procede de predictions de collision avec des obstacles au sol et d'alertes, notamment embarques sur un aeronef
CA2635817C (fr) * 2006-02-23 2016-05-31 Commonwealth Scientific And Industrial Research Organisation Systeme et procede permettant d'identifier les manoeuvres pour un vehicule dans des situations conflictuelles
FR2923641B1 (fr) * 2007-11-14 2011-03-18 Thales Sa Procede de protection par signalisation d'un aeronef contre les risques de collision avec le terrain lors de procedures a couloir de protection reduit avec fonctions specifiques
FR2932306B1 (fr) 2008-06-10 2010-08-20 Thales Sa Procede et dispositif d'aide a la navigation pour un aeronef vis-a-vis des obstacles.
FR2933523B1 (fr) * 2008-07-01 2014-04-18 Airbus France Procede et dispositif d'aide a la conduite d'un vehicule,en particulier d'un aeronef, pour l'evitement d'obstacles
ITRM20110651A1 (it) * 2010-12-20 2012-06-21 Selex Sistemi Integrati Spa Metodo di previsione rapida del profilo verticale della traiettoria per la gestione del traffico aereo, e relativo sistema atm.
DE102011010679A1 (de) * 2011-02-08 2012-08-09 Eads Deutschland Gmbh Unbemanntes Luftfahrzeug mit eingebautem Kollisionswarnsystem
US8942914B2 (en) * 2011-02-22 2015-01-27 General Electric Company Methods and systems for managing air traffic
FR2977948B1 (fr) 2011-07-12 2014-11-07 Eurocopter France Procede de pilotage automatique d'un aeronef a voilure tournante comprenant au moins une helice propulsive, dispositif de pilotage automatique et aeronef
CN103337199B (zh) * 2013-06-17 2015-06-17 西南民族大学 一种适用于机载防撞系统的多维机动防撞方法

Also Published As

Publication number Publication date
RU2683718C2 (ru) 2019-04-01
CA2881545A1 (fr) 2015-09-04
RU2015107383A (ru) 2016-09-27
US9418564B2 (en) 2016-08-16
CA2881545C (fr) 2022-11-01
RU2015107383A3 (fr) 2018-09-04
BR102015004715A2 (pt) 2017-03-21
FR3018364A1 (fr) 2015-09-11
US20150254991A1 (en) 2015-09-10
CN104900092A (zh) 2015-09-09
CN104900092B (zh) 2019-08-09

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