DE3861548D1 - Integriertes lagebestimmungssystem fuer flugzeuge. - Google Patents

Integriertes lagebestimmungssystem fuer flugzeuge.

Info

Publication number
DE3861548D1
DE3861548D1 DE8888400511T DE3861548T DE3861548D1 DE 3861548 D1 DE3861548 D1 DE 3861548D1 DE 8888400511 T DE8888400511 T DE 8888400511T DE 3861548 T DE3861548 T DE 3861548T DE 3861548 D1 DE3861548 D1 DE 3861548D1
Authority
DE
Germany
Prior art keywords
aircraft
positioning system
integrated positioning
integrated
positioning
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
DE8888400511T
Other languages
English (en)
Inventor
Benoit Pierson
Wladimir Osnowycz
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 Avionics SAS
Original Assignee
Thales Avionics 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 Thales Avionics SAS filed Critical Thales Avionics SAS
Application granted granted Critical
Publication of DE3861548D1 publication Critical patent/DE3861548D1/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
    • G05D1/08—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
    • 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
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
    • G01C21/188—Compensation of inertial measurements, e.g. for temperature effects for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
    • 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
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/166—Mechanical, construction or arrangement details of inertial navigation systems
    • 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
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
    • G01C21/185—Compensation of inertial measurements, e.g. for temperature effects for gravity

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Gyroscopes (AREA)
  • Navigation (AREA)
DE8888400511T 1987-04-28 1988-03-04 Integriertes lagebestimmungssystem fuer flugzeuge. Expired - Fee Related DE3861548D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8705985A FR2614694B1 (fr) 1987-04-28 1987-04-28 Centrale d'attitude integree pour aerodyne

Publications (1)

Publication Number Publication Date
DE3861548D1 true DE3861548D1 (de) 1991-02-21

Family

ID=9350553

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8888400511T Expired - Fee Related DE3861548D1 (de) 1987-04-28 1988-03-04 Integriertes lagebestimmungssystem fuer flugzeuge.

Country Status (3)

Country Link
EP (1) EP0292339B1 (de)
DE (1) DE3861548D1 (de)
FR (1) FR2614694B1 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2728339B1 (fr) * 1994-12-14 1997-04-04 Aerospatiale Procede et dispositif pour estimer des biais gyrometriques
AU777641B2 (en) * 1998-12-17 2004-10-28 Nec Tokin Corporation Orientation angle detector
FR2897715B1 (fr) * 2006-02-17 2008-05-30 Airbus France Sas Systeme de detection de desalignement pour capteur embarque
FR2955934B1 (fr) 2010-01-29 2012-03-09 Eurocopter France Estimation stabilisee en virage des angles d'assiettes d'un aeronef
FR2961305B1 (fr) 2010-06-14 2012-06-22 Eurocopter France Dispositif de mesure inertielle ameliore et aeronef comportant un tel dispositif
FR3030058B1 (fr) 2014-12-11 2016-12-09 Airbus Helicopters Dispositif redondant de capteurs de pilotage pour aeronef a voiture tournante
CN107077144B (zh) * 2016-09-09 2021-05-25 深圳市大疆创新科技有限公司 显示可移动装置的状态的方法、***和控制装置
IL253770B2 (en) * 2017-07-31 2023-02-01 Israel Aerospace Ind Ltd Determination of azimuth during flight

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4095271A (en) * 1977-04-20 1978-06-13 Sundstrand Data Control, Inc. Aircraft pitch attitude signal generator

Also Published As

Publication number Publication date
EP0292339B1 (de) 1991-01-16
FR2614694A1 (fr) 1988-11-04
EP0292339A1 (de) 1988-11-23
FR2614694B1 (fr) 1989-06-30

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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