DE3480738D1 - Geschwindigkeitssteuerung fuer ein flugzeug. - Google Patents

Geschwindigkeitssteuerung fuer ein flugzeug.

Info

Publication number
DE3480738D1
DE3480738D1 DE8484300287T DE3480738T DE3480738D1 DE 3480738 D1 DE3480738 D1 DE 3480738D1 DE 8484300287 T DE8484300287 T DE 8484300287T DE 3480738 T DE3480738 T DE 3480738T DE 3480738 D1 DE3480738 D1 DE 3480738D1
Authority
DE
Germany
Prior art keywords
airplane
speed control
speed
control
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
DE8484300287T
Other languages
English (en)
Inventor
Terry L Zweifel
Harry Miller
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 DE3480738D1 publication Critical patent/DE3480738D1/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, 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
    • G05D1/0638—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by combined action on the pitch and on the motors

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)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE8484300287T 1983-01-27 1984-01-18 Geschwindigkeitssteuerung fuer ein flugzeug. Expired - Lifetime DE3480738D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/461,357 US4641268A (en) 1983-01-27 1983-01-27 Cruise airspeed control for aircraft

Publications (1)

Publication Number Publication Date
DE3480738D1 true DE3480738D1 (de) 1990-01-18

Family

ID=23832245

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8484300287T Expired - Lifetime DE3480738D1 (de) 1983-01-27 1984-01-18 Geschwindigkeitssteuerung fuer ein flugzeug.

Country Status (5)

Country Link
US (1) US4641268A (de)
EP (1) EP0115401B1 (de)
JP (1) JPS59137300A (de)
CA (1) CA1199996A (de)
DE (1) DE3480738D1 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5031102A (en) * 1979-12-03 1991-07-09 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
US4662171A (en) * 1986-03-31 1987-05-05 The Boeing Company Automatic thrust restoration system
US4764872A (en) * 1986-07-16 1988-08-16 Honeywell Inc. Vertical flight path and airspeed control system for aircraft
US4805396A (en) * 1986-10-03 1989-02-21 Rockwell International Corporation Automatic fuel control and engine synchronizer system and apparatus
US5164993A (en) * 1991-11-25 1992-11-17 Eastman Kodak Company Method and apparatus for automatic tonescale generation in digital radiographic images
US20030176954A1 (en) * 2001-10-12 2003-09-18 Jaw Link C. Tracking and control of gas turbine engine component damage/life
US6814330B2 (en) * 2002-12-12 2004-11-09 The Boeing Company Method and computer program product for controlling the control effectors of an aerodynamic vehicle
US7031811B2 (en) * 2003-05-30 2006-04-18 The Boeing Company Fuel efficient airspeed trim
US6886786B1 (en) * 2003-10-10 2005-05-03 The Boeing Company Engine thrust management—new design architecture
US7769503B2 (en) * 2006-08-01 2010-08-03 Hal Gerard Wick Aircraft engine management for fuel conservation
US7706932B2 (en) * 2006-11-30 2010-04-27 Instituto Nacional de Tecnica Aeroespacial “Estaban Terradas” Method for controlling control parameters in an air vehicle and system of controlling an air vehicle
US7949440B2 (en) * 2006-12-22 2011-05-24 Embraer-Empresa Brasileira De Aeronautica S.A. Aircraft cruise speed control
US9085371B2 (en) * 2008-11-20 2015-07-21 The Boeing Company Automatic throttle roll angle compensation
US9058040B2 (en) * 2009-02-27 2015-06-16 The Boeing Company Automatic pilot pitch angle compensation
WO2018100494A1 (en) * 2016-11-30 2018-06-07 Bombardier Inc. Aircraft control system with residual error containment
US10946972B2 (en) 2017-12-08 2021-03-16 Pratt & Whitney Canada Corp. Method and system for controlling thrust of an engine
US11987375B2 (en) 2019-02-08 2024-05-21 Pratt & Whitney Canada Corp. System and method for operating engines of an aircraft in an asymmetric operating regime
US11725597B2 (en) 2019-02-08 2023-08-15 Pratt & Whitney Canada Corp. System and method for exiting an asymmetric engine operating regime
CN113955129B (zh) * 2021-09-16 2024-02-02 中国航空工业集团公司西安飞机设计研究所 一种自动油门马赫数控制方法
CN115059549B (zh) * 2022-06-16 2024-01-02 中国航发沈阳发动机研究所 一种防止大马赫数误操作油门杆的控制方法及系统

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2998946A (en) * 1959-05-14 1961-09-05 Sperry Rand Corp Aircraft automatic pilot
US3362661A (en) * 1965-06-14 1968-01-09 Ltv Aerospace Corp Autothrottle
US3510092A (en) * 1967-07-28 1970-05-05 Honeywell Inc Craft altitude control apparatus
US3624364A (en) * 1970-01-28 1971-11-30 Us Army Parallel speed stabilization system
US3945593A (en) * 1972-10-10 1976-03-23 Bodenseewerk Geratetechnik Gmbh Flight control apparatus
US3989208A (en) * 1972-11-16 1976-11-02 The Boeing Company Thrust and flight path control decoupling system
US3908934A (en) * 1973-12-03 1975-09-30 Sperry Rand Corp Programmed gain control for aircraft throttle control system
US4110605A (en) * 1977-02-25 1978-08-29 Sperry Rand Corporation Weight and balance computer apparatus for aircraft
US4312041A (en) * 1978-02-22 1982-01-19 Lear Siegler, Inc. Flight performance data computer system
US4277041A (en) * 1978-09-11 1981-07-07 Lockheed Corporation Aircraft cruise speed control system
US4357663A (en) * 1979-12-03 1982-11-02 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
US4490793A (en) * 1981-12-21 1984-12-25 Sperry Corporation Cruise speed control for aircraft performance management system

Also Published As

Publication number Publication date
JPS59137300A (ja) 1984-08-07
US4641268A (en) 1987-02-03
EP0115401B1 (de) 1989-12-13
CA1199996A (en) 1986-01-28
EP0115401A3 (en) 1985-07-31
EP0115401A2 (de) 1984-08-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition