DE69532632D1 - Flugzeug-Regelsystem für vertikale Position - Google Patents

Flugzeug-Regelsystem für vertikale Position

Info

Publication number
DE69532632D1
DE69532632D1 DE69532632T DE69532632T DE69532632D1 DE 69532632 D1 DE69532632 D1 DE 69532632D1 DE 69532632 T DE69532632 T DE 69532632T DE 69532632 T DE69532632 T DE 69532632T DE 69532632 D1 DE69532632 D1 DE 69532632D1
Authority
DE
Germany
Prior art keywords
control system
vertical position
airplane control
airplane
vertical
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
DE69532632T
Other languages
English (en)
Other versions
DE69532632T2 (de
Inventor
Guner Firuz
Dwight R Schaeffer
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=23752289&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE69532632(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE69532632D1 publication Critical patent/DE69532632D1/de
Publication of DE69532632T2 publication Critical patent/DE69532632T2/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

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)
DE69532632T 1995-05-15 1995-11-06 Flugzeug-Regelsystem für vertikale Position Expired - Lifetime DE69532632T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/441,284 US5695156A (en) 1995-05-15 1995-05-15 Aircraft vertical position control system
US441284 1995-05-15

Publications (2)

Publication Number Publication Date
DE69532632D1 true DE69532632D1 (de) 2004-04-08
DE69532632T2 DE69532632T2 (de) 2005-03-10

Family

ID=23752289

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69532632T Expired - Lifetime DE69532632T2 (de) 1995-05-15 1995-11-06 Flugzeug-Regelsystem für vertikale Position

Country Status (3)

Country Link
US (1) US5695156A (de)
EP (1) EP0743584B1 (de)
DE (1) DE69532632T2 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2754364B1 (fr) * 1996-10-03 1998-11-27 Aerospatiale Procede et dispositif de guidage vertical d'un aeronef
US6282466B1 (en) 1998-11-03 2001-08-28 The Boeing Company Method of automated thrust-based roll guidance limiting
US6711476B2 (en) 2001-09-27 2004-03-23 The Boeing Company Method and computer program product for estimating at least one state of a dynamic system
US6591169B2 (en) 2001-09-27 2003-07-08 The Boeing Company Method and computer program product for controlling the actuators of an aerodynamic vehicle
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
FR2909462B1 (fr) * 2006-12-05 2008-12-26 Airbus France Sas Procede et dispositif de controle actif du tangage d'un avion.
US8131410B2 (en) * 2007-06-15 2012-03-06 The Boeing Company Quiet climb crew interface
RU2451970C1 (ru) * 2011-02-09 2012-05-27 Федеральное Государственное Автономное Образовательное Учреждение Высшего Профессионального Образования "Дальневосточный Федеральный Университет" (Двфу) Способ управления движением динамического объекта по пространственной траектории
US8774985B2 (en) 2011-07-22 2014-07-08 The Boeing Company Systems and methods for generating a command trajectory
US8831799B1 (en) 2013-04-04 2014-09-09 The Boeing Company Flight director flare guidance
US9595200B2 (en) 2015-02-09 2017-03-14 The Boeing Company System and method for providing guidance during a flare maneuver of an aircraft
FR3044810A1 (fr) * 2015-12-04 2017-06-09 Airbus Operations Sas Systeme d’aide a la gestion du vol d’un aeronef lors d’une phase d’atterrissage.
US10481615B2 (en) * 2017-03-01 2019-11-19 Bell Textron Inc. Rotorcraft control mode transition smoothing
CN112558478B (zh) * 2020-12-08 2022-06-17 中国商用飞机有限责任公司 一种民机自动驾驶仪高度改平功能控制方法和系统

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3545703A (en) * 1967-11-01 1970-12-08 Bendix Corp System for controlling flight of aircraft to attain a predetermined altitude
GB1269044A (en) * 1968-04-11 1972-03-29 Elliott Brothers London Ltd Improvements in or relating to aircraft control systems
US3627236A (en) * 1970-06-30 1971-12-14 Sperry Rand Corp Automatic throttle control with airspeed anticipation
US4032093A (en) * 1975-06-27 1977-06-28 The Boeing Company Adaptive energy management for vertical speed control of an aircraft
US4114842A (en) * 1977-03-28 1978-09-19 Sperry Rand Corporation Acceleration limited preselect altitude capture and control
US4357663A (en) * 1979-12-03 1982-11-02 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
US4377848A (en) * 1980-10-16 1983-03-22 Sperry Corporation Altitude capture mode for aircraft automatic flight control system
WO1984001345A1 (en) * 1982-09-30 1984-04-12 Boeing Co Total energy based flight control system
US4633404A (en) * 1983-05-20 1986-12-30 Sperry Corporation Automatic deceleration of aircraft during descent
US5117362A (en) * 1989-12-15 1992-05-26 Honeywell Path capture forcing function generator for aircraft vertical axis control
US5079711A (en) * 1990-02-26 1992-01-07 The Boeing Company Aircraft high altitude vertical flight path and speed control system

Also Published As

Publication number Publication date
EP0743584B1 (de) 2004-03-03
DE69532632T2 (de) 2005-03-10
US5695156A (en) 1997-12-09
EP0743584A1 (de) 1996-11-20

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Legal Events

Date Code Title Description
8363 Opposition against the patent