DE69022209T2 - Automatisches Flugzeuglandesystem mit Vorkehrungen im Fall eines Triebwerkausfalls. - Google Patents

Automatisches Flugzeuglandesystem mit Vorkehrungen im Fall eines Triebwerkausfalls.

Info

Publication number
DE69022209T2
DE69022209T2 DE69022209T DE69022209T DE69022209T2 DE 69022209 T2 DE69022209 T2 DE 69022209T2 DE 69022209 T DE69022209 T DE 69022209T DE 69022209 T DE69022209 T DE 69022209T DE 69022209 T2 DE69022209 T2 DE 69022209T2
Authority
DE
Germany
Prior art keywords
precautions
event
aircraft landing
landing system
engine failure
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
DE69022209T
Other languages
English (en)
Other versions
DE69022209D1 (de
Inventor
Munir Orgun
Timothy Clark Mcroberts
Arvinder Sing Virdee
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of DE69022209D1 publication Critical patent/DE69022209D1/de
Application granted granted Critical
Publication of DE69022209T2 publication Critical patent/DE69022209T2/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
    • G05D1/0653—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
    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0072—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements to counteract a motor failure

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)
  • Feedback Control In General (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
DE69022209T 1990-01-26 1990-10-11 Automatisches Flugzeuglandesystem mit Vorkehrungen im Fall eines Triebwerkausfalls. Expired - Fee Related DE69022209T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/470,647 US5113346A (en) 1990-01-26 1990-01-26 Aircraft automatic landing system with engine out provisions

Publications (2)

Publication Number Publication Date
DE69022209D1 DE69022209D1 (de) 1995-10-12
DE69022209T2 true DE69022209T2 (de) 1996-02-01

Family

ID=23868439

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69022209T Expired - Fee Related DE69022209T2 (de) 1990-01-26 1990-10-11 Automatisches Flugzeuglandesystem mit Vorkehrungen im Fall eines Triebwerkausfalls.

Country Status (4)

Country Link
US (1) US5113346A (de)
EP (1) EP0438816B1 (de)
JP (1) JP3024804B2 (de)
DE (1) DE69022209T2 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5446666A (en) * 1994-05-17 1995-08-29 The Boeing Company Ground state-fly state transition control for unique-trim aircraft flight control system
US5657949A (en) * 1995-05-10 1997-08-19 The Boeing Company Method and apparatus for providing a dynamic thrust asymmetry rudder compensation command with no direct thrust measurement
US5761681A (en) * 1995-12-14 1998-06-02 Motorola, Inc. Method of substituting names in an electronic book
US5815407A (en) * 1995-12-14 1998-09-29 Motorola Inc. Method and device for inhibiting the operation of an electronic device during take-off and landing of an aircraft
US5893132A (en) * 1995-12-14 1999-04-06 Motorola, Inc. Method and system for encoding a book for reading using an electronic book
US5761682A (en) * 1995-12-14 1998-06-02 Motorola, Inc. Electronic book and method of capturing and storing a quote therein
US6126111A (en) * 1998-07-08 2000-10-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Emergency flight control system using one engine and fuel transfer
US6442451B1 (en) 2000-12-28 2002-08-27 Robotic Workspace Technologies, Inc. Versatile robot control system
CA2390487C (en) * 2001-06-11 2009-02-10 Robert D. Wiplinger Gear status indicator aircraft landing system
US20030014674A1 (en) * 2001-07-10 2003-01-16 Huffman James R. Method and electronic book for marking a page in a book
ATE394725T1 (de) * 2004-03-12 2008-05-15 Airbus Uk Ltd Modenunterdrückung in einem flugzeug
JP4328660B2 (ja) 2004-04-15 2009-09-09 富士重工業株式会社 航空機の自動離陸装置、自動着陸装置及び自動離着陸装置並びに航空機の自動離陸方法、自動着陸方法及び自動離着陸方法
FR2878288B1 (fr) * 2004-11-25 2007-01-19 Eurocopter France Procede et dispositif pour optimiser l'enveloppe de performances d'un turbomoteur
US7950987B2 (en) * 2005-09-23 2011-05-31 Honeywell International Inc. Aircraft cabin pressure control system and method that improves cabin pressurization during take-off
US20080133074A1 (en) * 2006-12-01 2008-06-05 Zyss Michael J Autonomous rollout control of air vehicle
US8508387B2 (en) * 2007-05-24 2013-08-13 Aviation Communication & Surveillance Systems Llc Systems and methods for aircraft windshear detection
US7671761B2 (en) * 2007-12-12 2010-03-02 The Boeing Company Method and system for calculating altitude above runway for an aircraft
EP2261116B1 (de) * 2009-06-09 2019-05-22 Sikorsky Aircraft Corporation Automatisches Trimmsystem für Fly-by-Wire-Flugzeuge mit einmaligen Trimmsteuerungen
FR2948468B1 (fr) * 2009-07-23 2011-09-16 Airbus Operations Sas Procede et dispositif d'aide au controle lateral d'aeronef lors d'une phase d'approche
US8903572B1 (en) * 2009-08-11 2014-12-02 The Boeing Company Aircraft landing evaluation system
US20110106345A1 (en) * 2009-11-03 2011-05-05 Takacs Robert S Low visibility landing system
US20150122945A1 (en) * 2013-11-03 2015-05-07 Peter Apostolos Kavounas Passenger aircraft with automatically deployable and/or retractable landing gear
CA2972495A1 (en) 2017-06-28 2018-12-28 Bombardier Inc. Sideslip guidance for one engine inoperative condition
CN109870900B (zh) * 2017-12-01 2022-10-04 上海航空电器有限公司 一种预防直升机起飞进近过程中横滚角过大的安全包线建立方法及应用
US11897596B2 (en) * 2020-07-21 2024-02-13 The Boeing Company Methods and apparatus for automatically extending aircraft wing flaps in response to detecting an excess energy steep descent condition
CN113238574B (zh) * 2021-05-08 2022-12-13 一飞(海南)科技有限公司 集群表演无人机落地检测控制方法、系统、终端及应用

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1561650A (en) * 1976-01-29 1980-02-27 Sperry Rand Corp Aircraft control system
US4354237A (en) * 1980-06-24 1982-10-12 The Boeing Company Method and apparatus for producing an aircraft flare path control signal
US4763266A (en) * 1982-12-27 1988-08-09 The Boeing Company Aircraft flight command and display system
US4538229A (en) * 1983-03-10 1985-08-27 Kavouras, Inc. System for preparing aircraft driftdown plans
US4841448A (en) * 1987-09-01 1989-06-20 Flight Dynamics, Inc. Windshear flight recovery command system
US4935682A (en) * 1988-08-11 1990-06-19 The Boeing Company Full authority engine-out control augmentation subsystem

Also Published As

Publication number Publication date
DE69022209D1 (de) 1995-10-12
JPH04331698A (ja) 1992-11-19
EP0438816B1 (de) 1995-09-06
JP3024804B2 (ja) 2000-03-27
EP0438816A1 (de) 1991-07-31
US5113346A (en) 1992-05-12

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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