GB0421231D0 - Aircraft mode suppression - Google Patents

Aircraft mode suppression

Info

Publication number
GB0421231D0
GB0421231D0 GBGB0421231.2A GB0421231A GB0421231D0 GB 0421231 D0 GB0421231 D0 GB 0421231D0 GB 0421231 A GB0421231 A GB 0421231A GB 0421231 D0 GB0421231 D0 GB 0421231D0
Authority
GB
United Kingdom
Prior art keywords
mode suppression
aircraft mode
aircraft
suppression
mode
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.)
Withdrawn
Application number
GBGB0421231.2A
Other versions
GB2411969A (en
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.)
Airbus Operations Ltd
Original Assignee
Airbus Operations Ltd
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 Airbus Operations Ltd filed Critical Airbus Operations Ltd
Publication of GB0421231D0 publication Critical patent/GB0421231D0/en
Priority to US11/078,646 priority Critical patent/US7357357B2/en
Priority to EP05251504A priority patent/EP1574923B1/en
Priority to DE602005006451T priority patent/DE602005006451D1/en
Priority to AT05251504T priority patent/ATE394725T1/en
Publication of GB2411969A publication Critical patent/GB2411969A/en
Withdrawn legal-status Critical Current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
    • G05D1/0083—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots to help an aircraft pilot in the rolling phase
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/17—Using electrical or electronic regulation means to control braking
    • B60T8/1701—Braking or traction control means specially adapted for particular types of vehicles
    • B60T8/1703—Braking or traction control means specially adapted for particular types of vehicles for aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/426—Braking devices providing an automatic sequence of braking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50—Steerable undercarriages; Shimmy-damping
    • B64C25/505—Shimmy damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transportation (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Regulating Braking Force (AREA)
GB0421231A 2004-03-12 2004-09-23 A system for control of an aircraft during breaking by reducing excitation of the aircraft modes Withdrawn GB2411969A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US11/078,646 US7357357B2 (en) 2004-03-12 2005-03-11 Aircraft mode suppression
EP05251504A EP1574923B1 (en) 2004-03-12 2005-03-11 Aircraft mode suppression
DE602005006451T DE602005006451D1 (en) 2004-03-12 2005-03-11 Mode suppression in an airplane
AT05251504T ATE394725T1 (en) 2004-03-12 2005-03-11 FASHION SUPPRESSION IN A PLANE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0405613.1A GB0405613D0 (en) 2004-03-12 2004-03-12 Aircraft mode suppression

Publications (2)

Publication Number Publication Date
GB0421231D0 true GB0421231D0 (en) 2004-10-27
GB2411969A GB2411969A (en) 2005-09-14

Family

ID=32117570

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB0405613.1A Ceased GB0405613D0 (en) 2004-03-12 2004-03-12 Aircraft mode suppression
GB0421231A Withdrawn GB2411969A (en) 2004-03-12 2004-09-23 A system for control of an aircraft during breaking by reducing excitation of the aircraft modes

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB0405613.1A Ceased GB0405613D0 (en) 2004-03-12 2004-03-12 Aircraft mode suppression

Country Status (1)

Country Link
GB (2) GB0405613D0 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201416842D0 (en) * 2014-09-24 2014-11-05 Rolls Royce Plc Aircraft
GB2540183A (en) 2015-07-08 2017-01-11 Airbus Operations Ltd Braking control system for an aircraft
FR3054335B1 (en) * 2016-07-25 2018-08-24 Airbus Operations METHOD AND DEVICE FOR REDUCING LOADS EXERCISED ON A STRUCTURAL ELEMENT OF AN AIRCRAFT.
US10525945B2 (en) * 2017-04-18 2020-01-07 Goodrich Corporation Antiskid brake control system with axle-mounted inertial sensor

Also Published As

Publication number Publication date
GB2411969A (en) 2005-09-14
GB0405613D0 (en) 2004-04-21

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)