DE60225198D1 - Flugzeugregelungssystem zum erreichen eines im flugplan vorhandenen punkts zur erforderten zeit - Google Patents

Flugzeugregelungssystem zum erreichen eines im flugplan vorhandenen punkts zur erforderten zeit

Info

Publication number
DE60225198D1
DE60225198D1 DE60225198T DE60225198T DE60225198D1 DE 60225198 D1 DE60225198 D1 DE 60225198D1 DE 60225198 T DE60225198 T DE 60225198T DE 60225198 T DE60225198 T DE 60225198T DE 60225198 D1 DE60225198 D1 DE 60225198D1
Authority
DE
Germany
Prior art keywords
signal
speed profile
sensitivity
required time
reaching
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
DE60225198T
Other languages
English (en)
Other versions
DE60225198T2 (de
Inventor
Jim R Rumbo
Brian E O'laughlin
Michael R Jackson
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.)
Honeywell International Inc
Original Assignee
Honeywell International 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 Honeywell International Inc filed Critical Honeywell International Inc
Application granted granted Critical
Publication of DE60225198D1 publication Critical patent/DE60225198D1/de
Publication of DE60225198T2 publication Critical patent/DE60225198T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
    • 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
    • G05D1/0005—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with arrangements to save energy

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Ultra Sonic Daignosis Equipment (AREA)
DE60225198T 2001-05-14 2002-05-14 Flugzeugregelungssystem zum erreichen eines im flugplan vorhandenen punkts zur erforderten zeit Expired - Lifetime DE60225198T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US855861 1986-04-24
US09/855,861 US6507782B1 (en) 2001-05-14 2001-05-14 Aircraft control system for reaching a waypoint at a required time of arrival
PCT/US2002/015222 WO2002093281A1 (en) 2001-05-14 2002-05-14 Aircraft control system for reaching a waypoint at a required time of arrival

Publications (2)

Publication Number Publication Date
DE60225198D1 true DE60225198D1 (de) 2008-04-03
DE60225198T2 DE60225198T2 (de) 2009-02-26

Family

ID=25322271

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60225198T Expired - Lifetime DE60225198T2 (de) 2001-05-14 2002-05-14 Flugzeugregelungssystem zum erreichen eines im flugplan vorhandenen punkts zur erforderten zeit

Country Status (5)

Country Link
US (1) US6507782B1 (de)
EP (1) EP1800197B1 (de)
AT (1) ATE386966T1 (de)
DE (1) DE60225198T2 (de)
WO (1) WO2002093281A1 (de)

Families Citing this family (70)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO317898B1 (no) * 2002-05-24 2004-12-27 Abb Research Ltd Fremgangsmate og system for a programmere en industrirobot
US7248963B2 (en) * 2003-03-25 2007-07-24 Baiada R Michael Method and system for aircraft flow management
US20050009891A1 (en) * 2003-07-09 2005-01-13 Lee Francis Y. Combination of SRC Kinase inhibitors and chemotherapeutic agents for the treatment of proliferative diseases
US20050075921A1 (en) * 2003-10-03 2005-04-07 Frederick Hayes-Roth Open community model for exchanging information in dynamic environments
FR2863372B1 (fr) * 2003-12-04 2006-02-10 Airbus France Procede et systeme de pilotage automatique d'un aeronef a l'approche d'une position de parachutage.
FR2866422B1 (fr) * 2004-02-16 2007-01-05 Airbus France Procede et dispositif de calcul d'une vitesse de consigne pour un aeronef.
US7366591B2 (en) * 2004-06-21 2008-04-29 Honeywell International, Inc. System and method for vertical flight planning
WO2006021815A1 (en) * 2004-07-14 2006-03-02 Bae Systems Plc Navigation display system
US7702427B1 (en) * 2004-07-30 2010-04-20 The United States Of America As Represented By The National Aeronautics And Space Administration (Nasa) Air traffic management evaluation tool
EP1770365B1 (de) 2005-09-30 2011-11-16 Saab Ab Verfahren zum Planen der Geschwindigkeit eines Fahrzeugs entlang einer Route
US7647139B2 (en) * 2005-12-02 2010-01-12 The Boeing Company Seamless air traffic control (ATC) datalink transfers
US20070150123A1 (en) * 2005-12-08 2007-06-28 The Boeing Company System and method for controlling the airspeed of an aircraft
FR2894705B1 (fr) * 2005-12-13 2010-11-19 Thales Sa Systeme de gestion de vol d'un aeronef
US7603228B2 (en) * 2006-05-25 2009-10-13 Ford Global Technologies, Llc Haptic apparatus and coaching method for improving vehicle fuel economy
FR2907952B1 (fr) * 2006-10-26 2008-12-19 Airbus France Sa Procede et dispositif d'aide au guidage d'un aeronef le long d'une trajectoire de vol.
FR2907953B1 (fr) * 2006-10-26 2008-12-19 Airbus France Sa Systeme de guidage d'un aeronef.
FR2913780B1 (fr) * 2007-03-13 2014-07-18 Airbus France Procede et dispositif d'aide au guidage d'un aeronef
FR2916842B1 (fr) 2007-06-01 2010-02-26 Thales Sa Procede d'optimisation d'un plan de vol
US8108136B2 (en) * 2007-08-09 2012-01-31 Ford Global Technologies, Llc. Driver advisory system for fuel economy improvement of a hybrid electric vehicle
US9726088B2 (en) * 2007-10-30 2017-08-08 Ford Global Technologies, Llc System and method for obtaining an adjustable accelerator pedal response in a vehicle powertrain
FR2923032B1 (fr) * 2007-10-31 2010-11-12 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef en vue d'une phase de descente.
US9257047B2 (en) * 2007-12-12 2016-02-09 The Boeing Company Computation of new aircraft trajectory using time factor
FR2930053B1 (fr) * 2008-04-14 2013-09-20 Airbus France Procede et dispositif de guidage d'un aeronef
US20090265049A1 (en) * 2008-04-22 2009-10-22 Honeywell International, Inc. Aircraft system emissions and noise estimation mechanism
US9829341B1 (en) * 2008-06-26 2017-11-28 Rockwell Collins, Inc. System and method for providing flight cues for the navigation function required time of arrival (RTA)
FR2935495B1 (fr) * 2008-08-29 2010-09-10 Thales Sa Systeme et procede de calcul des predictions de vol par sections verticales
US8010267B2 (en) * 2008-10-31 2011-08-30 General Electric Company Methods and system for time of arrival control using available speed authority
FR2938327B1 (fr) * 2008-11-07 2010-12-10 Thales Sa Procede pour la determination de la vitesse d'un aeronef
US8150588B2 (en) 2008-11-25 2012-04-03 General Electric Company Methods and system for time of arrival control using time of arrival uncertainty
FR2938939B1 (fr) * 2008-11-25 2015-10-02 Thales Sa Procede d'aide a la gestion du vol d'un aeronef en vue de tenir une contrainte de temps
FR2942328B1 (fr) 2009-02-17 2011-02-25 Thales Sa Procede d'aide a l'elaboration de la strategie de vitesse d'un aeronef en vue de tenir une contrainte de temps
US8311780B2 (en) * 2009-04-23 2012-11-13 Honeywell International Inc. Enhanced prediction of atmospheric parameters
EP2282247B1 (de) * 2009-05-05 2019-07-10 The Boeing Company Vierdimensionale Lenkung eines Flugzeugs
FR2946161B1 (fr) * 2009-05-29 2016-08-26 Thales Sa Procede d'elaboration continue et adaptative d'une consigne de vitesse pour la tenue d'un rta par un aeronef
US8321071B2 (en) 2009-07-31 2012-11-27 Ge Aviation Systems, Llc Method and system for vertical navigation using time-of-arrival control
US8515596B2 (en) * 2009-08-18 2013-08-20 Honeywell International Inc. Incremental position-based guidance for a UAV
FR2949577B1 (fr) * 2009-08-28 2012-03-16 Thales Sa Procede d'aide a la gestion d'un vol en vue de tenir une contrainte de temps
FR2949576B1 (fr) * 2009-08-28 2012-01-27 Thales Sa Procede d'aide a la gestion d'un vol en vue de tenir une contrainte de temps
DE102009052047B4 (de) * 2009-11-05 2014-01-16 Airbus Operations Gmbh Regeleinheit und Verfahren zum Regeln der Versorgung eines Fahrzeugs mit mehreren Treibstoffen
US20110118908A1 (en) * 2009-11-18 2011-05-19 The Boeing Company Methods and systems for management of airplane speed profile
FR2953302B1 (fr) * 2009-11-27 2012-08-10 Thales Sa Procede de planification, de calcul de trajectoire, de predictions et de guidage pour le respect d'une contrainte de temps de passage d'un aeronef
US8688363B2 (en) * 2010-04-30 2014-04-01 Honeywell International Inc. Aircraft systems and methods with active deceleration control
US8311687B2 (en) 2010-07-30 2012-11-13 Ge Aviation Systems Llc Method and system for vertical navigation using time-of-arrival control
US9761148B2 (en) 2010-08-03 2017-09-12 Honeywell International Inc. Airborne separation assurance system and required time of arrival function cooperation
ES2485294T3 (es) * 2010-08-24 2014-08-13 The Boeing Company Guiado en cuatro dimensiones de una aeronave
US9342076B2 (en) * 2010-08-25 2016-05-17 Valmont Industries, Inc. Adjustable speed irrigation system and method of use
US8406939B2 (en) 2010-09-03 2013-03-26 Honeywell International Inc. Systems and methods for RTA control of multi-segment flight plans with smooth transitions
US8818576B2 (en) * 2010-09-30 2014-08-26 The Boeing Company Tailored arrivals allocation system trajectory predictor
US8583352B2 (en) 2010-11-22 2013-11-12 Ge Aviation Systems, Llc Method and system for hold path computation to meet required hold departure time
US9087450B2 (en) 2011-05-17 2015-07-21 Innovative Solutions And Support, Inc. Upgraded flight management system and method of providing the same
US9709992B2 (en) 2011-05-17 2017-07-18 Innovative Solutions & Support, Inc. Upgraded flight management system for autopilot control and method of providing the same
US8872081B2 (en) * 2011-11-01 2014-10-28 Ge Aviation Systems Llc Methods for adjusting a relative navigation system
US8788189B2 (en) * 2012-08-31 2014-07-22 Honeywell International Inc. Aircraft control system and method for reaching a waypoint at a required time of arrival
US10013236B2 (en) 2013-03-06 2018-07-03 The Boeing Company Real-time adaptive speed scheduler
US9047763B2 (en) 2013-03-15 2015-06-02 Honeywell International Inc. Methods and systems for representing time of arrival information on a cockpit display
EP2804066B1 (de) 2013-05-17 2019-08-28 The Boeing Company Verfahren und System zur Flugzeugführung
US9026275B1 (en) * 2013-07-24 2015-05-05 Shih-Yih Young In-flight generation of RTA-compliant optimal profile descent paths
FR3012230B1 (fr) * 2013-10-17 2016-01-01 Airbus Operations Sas Procede et dispositif de revision d'une phase de vol a basse altitude d'une trajectoire de vol d'un aeronef.
FR3016975B1 (fr) 2014-01-24 2016-01-15 Thales Sa Procede d'aide a la navigation pour la tenue de contraintes temporelles multiples
US9625261B2 (en) 2014-09-04 2017-04-18 Honeywell International Inc. System and method for managing speed constraints during required time of arrival operations
US10144505B2 (en) * 2015-05-18 2018-12-04 The Boeing Company Aircraft flight control using a required time of arrival index
EP3109724B1 (de) 2015-06-26 2022-02-09 The Boeing Company Verfahren und system zur steuerung eines flugs eines flugzeugs mit einer ankunftszeitbeschränkung
EP3109723B1 (de) 2015-06-26 2018-10-24 The Boeing Company Verfahren und system zur steuerung des fluges eines flugzeuges mit mindestens zwei erforderlichen ankunftszeitbeschränkungen
GB2529551B (en) * 2015-07-22 2016-07-20 Via Tech Ltd Method for detecting conflicts between aircraft
US9540005B1 (en) 2016-03-28 2017-01-10 Honeywell International Inc. Aircraft systems and methods with multiple SAP speed profiles
US10528043B2 (en) * 2017-07-25 2020-01-07 Honeywell International Inc. Systems and methods for maximizing time reliability and fuel-efficiency for an aircraft to meet constraints associated with a required time of arrival (RTA)
US10388170B2 (en) 2017-08-14 2019-08-20 Honeywell International Inc. Speed-constrained flight management methods and systems
US11120694B2 (en) 2018-12-19 2021-09-14 Honeywell International Inc. Systems and methods for providing thrust guidance related to flight path angle
US11299285B2 (en) * 2018-12-20 2022-04-12 Honeywell International Inc. Systems and methods for providing throttle guidance as a function of flight path acceleration
US11587447B2 (en) 2020-01-23 2023-02-21 Honeywell International Inc. Dynamically modifiable parameters in required time of arrival (RTA) regions of an assigned flight path

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4760530A (en) * 1986-06-17 1988-07-26 Honeywell Inc. Flight management system providing minimum total cost
US5051910A (en) * 1989-10-16 1991-09-24 Honeywell Inc. Wind forecast error compensation for 4-D guidance in a aircraft flight management system
US5121325A (en) 1990-04-04 1992-06-09 Smiths Industries Aerospace & Defense Systems, Inc. Required time of arrival (RTA) control system
US5408413A (en) 1993-08-03 1995-04-18 Honeywell Inc. Apparatus and method for controlling an optimizing aircraft performance calculator to achieve time-constrained navigation
FR2749933B1 (fr) 1996-06-14 1998-09-11 Sextant Avionique Procede pour la gestion de la vitesse air en vue du respect des contraintes de temps d'un aerodyne dans un environnement meteorologique evolutif

Also Published As

Publication number Publication date
EP1800197A1 (de) 2007-06-27
EP1800197B1 (de) 2008-02-20
DE60225198T2 (de) 2009-02-26
WO2002093281A1 (en) 2002-11-21
ATE386966T1 (de) 2008-03-15
US6507782B1 (en) 2003-01-14

Similar Documents

Publication Publication Date Title
DE60225198D1 (de) Flugzeugregelungssystem zum erreichen eines im flugplan vorhandenen punkts zur erforderten zeit
ATE257970T1 (de) System zur flugsteuerung eines kreismanövers zum landen
WO2018233164A8 (zh) 飞行控制方法、信息处理装置、程序及记录介质
ATE354784T1 (de) Verfahren und vorrichtung zur bereitstellung einer flugbahn für ein flugzeug
GB0613083D0 (en) A Multilateration System and Method
EP2703926A3 (de) Flugzeugsteuersystem und Verfahren zum Erreichen eines Wegpunktes zu einer erforderlichen Ankunftszeit
US20080103647A1 (en) Guidance system for an aircraft
ATE532453T1 (de) System zur kontrolle einer vorrichtung in vivo
WO2002041131A3 (en) A method and system for entering data within a flight plan entry field
GB2437030A (en) Precision approach guidance system and associated method
WO2009082785A8 (en) A method and system of controlling air traffic
DE602007001023D1 (de) Gleitanflugverfahren für maximale Vorhersagbarkeit
WO2011056795A3 (en) Low visibility landing system and method
ATE353136T1 (de) Verfahren und vorrichtung zum abändern eines flugplanes eines flugzeuges
DE602005005870D1 (de) Verfahren und Vorrichtung zur Sollgeschwindigkeitsberechnung für ein Luftfahrzeug
EP2177966A3 (de) Systeme und Verfahren zur Navigation eines unbemannten Luftfahrzeugs
WO2010017044A3 (en) Four-dimensional navigation of an aircraft
WO2002005246A3 (en) Multisource target correlation
DE60310577D1 (de) Lenkhilfesystem für höhe und horizontalgeschwindigkeit, senkrechte zur vertikalen eines flugzeugs und damit ausgestattetes flugzeug
ATE495096T1 (de) Verfahren und einrichtung zur höhenflossentrimmung bei einem flugzeug
DE60125187D1 (de) Flugzeuglandewinkelüberwachungseinrichtung
ATE326387T1 (de) Verfahren und vorrichtung zum bestimmen eines endanflugpfades eines flugzeuges für einen nicht- präzisions-landeanflug eines flugzeuges
ATE535898T1 (de) Führungseinrichtung und verfahren zur anflugführung von luftfahrzeugen
WO2007093697A3 (fr) Procede et systeme d'aide au pilotage d'un aeronef
DE60302643D1 (de) Verfahren und Vorrichtung zur Ansteuerung von Flugzeugrudern

Legal Events

Date Code Title Description
8364 No opposition during term of opposition