DE68913559D1 - Führung eines Flugzeuges mit einem Inertialsensor im Bereich der Windscherung. - Google Patents

Führung eines Flugzeuges mit einem Inertialsensor im Bereich der Windscherung.

Info

Publication number
DE68913559D1
DE68913559D1 DE89100225T DE68913559T DE68913559D1 DE 68913559 D1 DE68913559 D1 DE 68913559D1 DE 89100225 T DE89100225 T DE 89100225T DE 68913559 T DE68913559 T DE 68913559T DE 68913559 D1 DE68913559 D1 DE 68913559D1
Authority
DE
Germany
Prior art keywords
aircraft
guiding
area
inertial sensor
wind shear
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 - Fee Related
Application number
DE89100225T
Other languages
English (en)
Other versions
DE68913559T2 (de
Inventor
Terry L Zweifel
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 Inc
Original Assignee
Honeywell 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 Inc filed Critical Honeywell Inc
Application granted granted Critical
Publication of DE68913559D1 publication Critical patent/DE68913559D1/de
Publication of DE68913559T2 publication Critical patent/DE68913559T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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, 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
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind

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)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
DE68913559T 1988-01-11 1989-01-07 Führung eines Flugzeuges mit einem Inertialsensor im Bereich der Windscherung. Expired - Fee Related DE68913559T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/141,752 US4893245A (en) 1988-01-11 1988-01-11 Windshear guidance for aircraft having inertial sensor

Publications (2)

Publication Number Publication Date
DE68913559D1 true DE68913559D1 (de) 1994-04-14
DE68913559T2 DE68913559T2 (de) 1994-08-11

Family

ID=22497069

Family Applications (1)

Application Number Title Priority Date Filing Date
DE68913559T Expired - Fee Related DE68913559T2 (de) 1988-01-11 1989-01-07 Führung eines Flugzeuges mit einem Inertialsensor im Bereich der Windscherung.

Country Status (6)

Country Link
US (1) US4893245A (de)
EP (1) EP0324393B1 (de)
JP (1) JPH01309894A (de)
CA (1) CA1334862C (de)
DE (1) DE68913559T2 (de)
ES (1) ES2051314T3 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5089968A (en) * 1990-01-26 1992-02-18 The Boeing Company Ground effects compensated real time aircraft body angle of attack estimation
FR2760268B1 (fr) * 1997-03-03 1999-04-30 Aerospatiale Procede et dispositif pour verifier la coherence des mesures d'une sonde d'incidence
US6273370B1 (en) * 1999-11-01 2001-08-14 Lockheed Martin Corporation Method and system for estimation and correction of angle-of-attack and sideslip angle from acceleration measurements
FR2874204B1 (fr) * 2004-08-13 2007-12-14 Airbus France Sas Systeme de commande de vol electriques pour les gouvernes de profondeur d'un aeronef
US7557735B1 (en) 2006-09-05 2009-07-07 Rockwell Collins, Inc. Predictive and reactive windshear detection system and method
US8508387B2 (en) * 2007-05-24 2013-08-13 Aviation Communication & Surveillance Systems Llc Systems and methods for aircraft windshear detection
JP5771893B2 (ja) * 2009-11-20 2015-09-02 国立研究開発法人宇宙航空研究開発機構 乱気流抑制制御方法
JP6114075B2 (ja) * 2013-03-07 2017-04-12 三菱航空機株式会社 航空機の警報システム、及び、航空機

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3791208A (en) * 1971-03-16 1974-02-12 Sperry Rand Corp Angle of attack computer
US4261537A (en) * 1979-02-28 1981-04-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Velocity vector control system augmented with direct lift control
US4373184A (en) * 1979-12-26 1983-02-08 The Boeing Company Vertical flight path steering system for aircraft
US4442490A (en) * 1980-09-26 1984-04-10 S-Tec Corporation Aircraft pitch stabilization apparatus
FR2511146B1 (fr) * 1981-08-07 1986-07-25 British Aerospace Instrument de navigation
EP0120855B1 (de) * 1982-09-30 1989-01-25 The Boeing Company Flugregelsystem auf basis totaler energie
US4593285A (en) * 1983-05-06 1986-06-03 Sperry Corporation Windshear detection and warning system with evasion command
US4857922A (en) * 1983-05-06 1989-08-15 Honeywell Inc. Windshear detection and warning system with evasion command
US4728951A (en) * 1985-10-16 1988-03-01 Honeywell Inc. Vertical windshear detection for aircraft
DE3582074D1 (de) * 1985-12-18 1991-04-11 Boeing Co Flugregel- und anzeigesystem fuer windscherung.
DE3578659D1 (de) * 1985-12-18 1990-08-16 Boeing Co Flugregel- und anzeigesystem fuer windscherung.
US4725811A (en) * 1986-02-13 1988-02-16 Sundstrand Data Control, Inc. Wind shear detection and alerting system
US4797674A (en) * 1986-02-28 1989-01-10 Honeywill Inc. Flight guidance system for aircraft in windshear
EP0317678B1 (de) * 1987-11-27 1993-03-24 Honeywell Inc. Optimale Steuerung eines Flugzeuges im Bereich der Windscherung

Also Published As

Publication number Publication date
US4893245A (en) 1990-01-09
DE68913559T2 (de) 1994-08-11
EP0324393A2 (de) 1989-07-19
ES2051314T3 (es) 1994-06-16
CA1334862C (en) 1995-03-21
JPH01309894A (ja) 1989-12-14
EP0324393A3 (en) 1990-06-06
EP0324393B1 (de) 1994-03-09

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee