CA2773702C - Systeme de commande pour vehicules - Google Patents

Systeme de commande pour vehicules Download PDF

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Publication number
CA2773702C
CA2773702C CA2773702A CA2773702A CA2773702C CA 2773702 C CA2773702 C CA 2773702C CA 2773702 A CA2773702 A CA 2773702A CA 2773702 A CA2773702 A CA 2773702A CA 2773702 C CA2773702 C CA 2773702C
Authority
CA
Canada
Prior art keywords
velocity
relative
aircraft
moving vehicle
vehicle
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.)
Expired - Lifetime
Application number
CA2773702A
Other languages
English (en)
Other versions
CA2773702A1 (fr
Inventor
Kenneth E. Builta
James E. Harris
Bryan P. Honza
Jeffrey W. Epp
Kynn J. Schulte
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.)
Bell Helicopter Textron Inc
Original Assignee
Bell Helicopter Textron Inc
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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Priority to CA2773702A priority Critical patent/CA2773702C/fr
Priority to CA2788512A priority patent/CA2788512C/fr
Priority claimed from CA2555836A external-priority patent/CA2555836C/fr
Publication of CA2773702A1 publication Critical patent/CA2773702A1/fr
Application granted granted Critical
Publication of CA2773702C publication Critical patent/CA2773702C/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • G01C23/005—Flight directors
    • 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
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G05D1/0684—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing on a moving platform, e.g. aircraft carrier
    • 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
    • G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
    • G08G5/22—Arrangements for acquiring, generating, sharing or displaying traffic information located on the ground
    • 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
    • G08G5/26—Transmission of traffic-related information between aircraft and ground stations
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/70—Arrangements for monitoring traffic-related situations or conditions
    • G08G5/72—Arrangements for monitoring traffic-related situations or conditions for monitoring traffic
    • G08G5/723—Arrangements for monitoring traffic-related situations or conditions for monitoring traffic from the aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G7/00—Traffic control systems for simultaneous control of two or more different kinds of craft

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)

Abstract

Un système servant à commander le vol d'un aéronef comporte des capteurs (37, 43), un récepteur (45) et un système de commande numérique (57), tous étant à bord de l'aéronef. Les capteurs (37, 43) déterminent la position de l'aéronef par rapport à la Terre et le mouvement inertiel de l'aéronef. Le récepteur (45) reçoit les données transmises (51, 55) communiquant la position et le mouvement d'un véhicule de référence par rapport à la Terre. Le système de commande (57) calcule la position et la vitesse de l'aéronef par rapport au véhicule de référence à l'aide des données des capteurs (37,43) et du récepteur (45) puis commande les dispositifs de commande de vol (33) de l'aéronef pour les manuvres de l'aéronef de manière à maintenir une position et/ou une vitesse sélectionnées par rapport au véhicule de référence. Le système permet l'utilisation d'interfaces utilisateurs graphiques ou tactiles.
CA2773702A 2004-03-25 2004-03-25 Systeme de commande pour vehicules Expired - Lifetime CA2773702C (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CA2773702A CA2773702C (fr) 2004-03-25 2004-03-25 Systeme de commande pour vehicules
CA2788512A CA2788512C (fr) 2004-03-25 2004-03-25 Systeme de commande pour vehicules

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CA2773702A CA2773702C (fr) 2004-03-25 2004-03-25 Systeme de commande pour vehicules
CA2555836A CA2555836C (fr) 2004-03-25 2004-03-25 Systeme de commande pour vehicules

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CA2555836A Division CA2555836C (fr) 2004-03-25 2004-03-25 Systeme de commande pour vehicules

Publications (2)

Publication Number Publication Date
CA2773702A1 CA2773702A1 (fr) 2005-11-03
CA2773702C true CA2773702C (fr) 2014-07-22

Family

ID=46206218

Family Applications (2)

Application Number Title Priority Date Filing Date
CA2788512A Expired - Lifetime CA2788512C (fr) 2004-03-25 2004-03-25 Systeme de commande pour vehicules
CA2773702A Expired - Lifetime CA2773702C (fr) 2004-03-25 2004-03-25 Systeme de commande pour vehicules

Family Applications Before (1)

Application Number Title Priority Date Filing Date
CA2788512A Expired - Lifetime CA2788512C (fr) 2004-03-25 2004-03-25 Systeme de commande pour vehicules

Country Status (1)

Country Link
CA (2) CA2788512C (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8200375B2 (en) 2008-02-12 2012-06-12 Stuckman Katherine C Radio controlled aircraft, remote controller and methods for use therewith
DE102009041652B4 (de) * 2009-09-17 2017-12-28 Airbus Defence and Space GmbH -Verfahren zum automatischen Landen eines Luftfahrzeugs
FR2984267B1 (fr) * 2011-12-19 2015-08-28 Airbus Operations Sas Systeme de commande de l'energie d'un vehicule
CN105938369B (zh) 2013-06-25 2018-11-02 深圳市大疆创新科技有限公司 飞行器的控制系统及控制方法
US9830828B2 (en) 2015-03-24 2017-11-28 Honeywell International Inc. Systems and method for AIS transponder integration with ILS/VOR receivers
CN104898699B (zh) * 2015-05-28 2020-03-17 小米科技有限责任公司 飞行控制方法及装置、电子设备

Also Published As

Publication number Publication date
CA2788512C (fr) 2014-05-20
CA2788512A1 (fr) 2005-11-03
CA2773702A1 (fr) 2005-11-03

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Effective date: 20240325