GB1528939A - Aircraft control systems - Google Patents

Aircraft control systems

Info

Publication number
GB1528939A
GB1528939A GB52358/75A GB5235875A GB1528939A GB 1528939 A GB1528939 A GB 1528939A GB 52358/75 A GB52358/75 A GB 52358/75A GB 5235875 A GB5235875 A GB 5235875A GB 1528939 A GB1528939 A GB 1528939A
Authority
GB
United Kingdom
Prior art keywords
pitch
attitude
control
comparator
signal
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
Application number
GB52358/75A
Other languages
English (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.)
Unisys Corp
Original Assignee
Sperry Rand Corp
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 Sperry Rand Corp filed Critical Sperry Rand Corp
Publication of GB1528939A publication Critical patent/GB1528939A/en
Expired 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
    • G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Feedback Control In General (AREA)
GB52358/75A 1975-01-23 1975-12-22 Aircraft control systems Expired GB1528939A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/543,210 US3945590A (en) 1975-01-23 1975-01-23 Semi-automatic takeoff control system for aircraft

Publications (1)

Publication Number Publication Date
GB1528939A true GB1528939A (en) 1978-10-18

Family

ID=24167049

Family Applications (1)

Application Number Title Priority Date Filing Date
GB52358/75A Expired GB1528939A (en) 1975-01-23 1975-12-22 Aircraft control systems

Country Status (7)

Country Link
US (1) US3945590A (enExample)
JP (1) JPS5187299A (enExample)
CA (1) CA1050138A (enExample)
DE (1) DE2601827A1 (enExample)
FR (1) FR2298822A1 (enExample)
GB (1) GB1528939A (enExample)
SE (1) SE7514191L (enExample)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE2924742C2 (de) * 1979-06-20 1983-12-08 Dornier Gmbh, 7990 Friedrichshafen Großflugzeug, insbesondere in Schulterdeckerbauart
US4357663A (en) * 1979-12-03 1982-11-02 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
US4471439A (en) * 1982-09-20 1984-09-11 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
EP0368989A4 (en) * 1988-04-11 1990-06-26 Sundstrand Data Control SYSTEM FOR WINCH SHEAR INTERCEPTIONS WITH STABLE PROTECTION.
WO1995012153A1 (en) * 1992-10-06 1995-05-04 Honeywell Inc. Position dependent rate dampening in an active hand controller
FR2711257B1 (fr) * 1993-10-14 1995-12-22 Aerospatiale Système de commande de vol électrique pour avion avec protection en assiette au décollage.
US5901927A (en) * 1996-07-18 1999-05-11 Honeywell Inc. Ground strike protection function for aircraft autopilot
US6422517B1 (en) 1999-12-02 2002-07-23 Boeing Company Aircraft tailstrike avoidance system
FR2817535B1 (fr) 2000-12-06 2003-03-21 Eads Airbus Sa Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef durant le decollage
FR2859174B1 (fr) * 2003-08-26 2006-03-10 Airbus France Procede et dispositif pour controler l'assiette d'un avion
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
FR2909461B1 (fr) * 2006-12-05 2014-08-22 Airbus France Procede et dispositif de decollage automatique d'un avion.
FR2949219B1 (fr) * 2009-08-21 2011-09-16 Ratier Figeac Soc Dispositif de pilotage d'un vehicule et procede d'assistance motorisee et de controle d'un tel dispositif de pilotage
EP2490936B2 (en) 2009-10-19 2020-07-22 BAE Systems PLC Tactile cueing apparatus
US8793040B2 (en) * 2011-06-10 2014-07-29 Embraer S.A. Climb-optimized auto takeoff system
CN104691742B (zh) * 2013-12-10 2017-07-25 中国航空工业第六一八研究所 一种飞翼布局无人飞机应用阻力方向舵的控制方法
EP2913265B1 (en) * 2014-02-27 2019-07-17 Goodrich Actuation Systems SAS Stability and control augmentation system
CN105334735A (zh) * 2015-11-13 2016-02-17 成都飞机工业（集团）有限责任公司 一种基于角速率的飞翼布局无人机控制律
CN108319288A (zh) * 2016-01-26 2018-07-24 深圳市大疆创新科技有限公司 无人机及其飞行控制方法与系统
US11226639B2 (en) 2016-09-23 2022-01-18 Yaborã Indústria Aeronáutica S.A. Enhanced take-off system
CN106681344B (zh) * 2016-12-26 2019-08-27 湖南纳雷科技有限公司 一种用于飞行器的高度控制方法及控制系统
US11841713B2 (en) * 2020-01-07 2023-12-12 Gulfstream Aerospace Corporation Controllers and aircraft with takeoff stall protection system
US12493302B2 (en) * 2020-06-25 2025-12-09 Embraer S.A. Longitudinal trim control movement during takeoff rotation
US12441468B2 (en) * 2022-11-18 2025-10-14 Brown University Bio-inspired flapping wing/fin robotic platform

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3313152A (en) * 1963-05-06 1967-04-11 Giannini Controls Corp Flight control system
GB1156324A (en) * 1965-07-14 1969-06-25 Elliott Brothers London Ltd Improvements relating to Take-Off Director Systems for Aircraft
GB1204481A (en) * 1966-07-29 1970-09-09 Elliott Brothers London Ltd Improvements relating to take-off director systems for aircraft
US3848833A (en) * 1972-07-14 1974-11-19 Sperry Rand Corp Aircraft automatic flight control system

Also Published As

Publication number Publication date
US3945590A (en) 1976-03-23
FR2298822A1 (fr) 1976-08-20
CA1050138A (en) 1979-03-06
SE7514191L (sv) 1976-07-26
DE2601827A1 (de) 1976-07-29
JPS5187299A (enExample) 1976-07-30

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee