DE2223975B2 - Regelvorrichtung fur die Grundgeschwindigkeit eines Hubschraubers - Google Patents

Regelvorrichtung fur die Grundgeschwindigkeit eines Hubschraubers

Info

Publication number
DE2223975B2
DE2223975B2 DE2223975A DE2223975A DE2223975B2 DE 2223975 B2 DE2223975 B2 DE 2223975B2 DE 2223975 A DE2223975 A DE 2223975A DE 2223975 A DE2223975 A DE 2223975A DE 2223975 B2 DE2223975 B2 DE 2223975B2
Authority
DE
Germany
Prior art keywords
signal
acceleration
helicopter
summing circuit
speed
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Withdrawn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
DE2223975A
Other languages
German (de)
English (en)
Other versions
DE2223975A1 (de
Inventor
Don Louis Fairfield Adams
Louis Saxon Monroe Cotton
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.)
RTX Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE2223975A1 publication Critical patent/DE2223975A1/de
Publication of DE2223975B2 publication Critical patent/DE2223975B2/de
Withdrawn legal-status Critical Current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
    • G05D1/04—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
    • G05D1/0669—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off specially adapted for vertical take-off
    • 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
    • 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
    • G05D1/0623—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the pitch

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)
DE2223975A 1971-05-20 1972-05-17 Regelvorrichtung fur die Grundgeschwindigkeit eines Hubschraubers Withdrawn DE2223975B2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14657571A 1971-05-20 1971-05-20

Publications (2)

Publication Number Publication Date
DE2223975A1 DE2223975A1 (de) 1973-02-15
DE2223975B2 true DE2223975B2 (de) 1980-04-10

Family

ID=22518017

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2223975A Withdrawn DE2223975B2 (de) 1971-05-20 1972-05-17 Regelvorrichtung fur die Grundgeschwindigkeit eines Hubschraubers

Country Status (6)

Country Link
US (1) US3724786A (member.php)
CA (1) CA973953A (member.php)
DE (1) DE2223975B2 (member.php)
FR (1) FR2139096B1 (member.php)
GB (1) GB1340448A (member.php)
IT (1) IT959696B (member.php)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4646243A (en) * 1983-01-13 1987-02-24 The Boeing Company Apparatus for determining the groundspeed rate of an aircraft
US4594592A (en) * 1984-01-09 1986-06-10 Greene Leonard M Airplane safe take-off rotation indicator
US8219267B2 (en) * 2010-05-27 2012-07-10 Honeywell International Inc. Wind estimation for an unmanned aerial vehicle
NO344081B1 (no) * 2012-04-02 2019-09-02 FLIR Unmanned Aerial Systems AS Fremgangsmåte og anordning for å navigere et luftfartøy
US11312480B2 (en) 2018-06-01 2022-04-26 Textron Innovations Inc. System and method for controlling rotorcraft
EP3677505B1 (en) * 2019-01-02 2024-03-20 Textron Innovations Inc. System and method for controlling rotorcraft
US12503224B2 (en) 2024-01-08 2025-12-23 Lockheed Martin Corporation Thrust control for ground navigation of aerial vehicles

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3071335A (en) * 1958-10-03 1963-01-01 United Aircraft Corp Flight control system
DE1481549B2 (de) * 1966-07-26 1971-09-09 Bodenseewerk Geratetechnik GmbH, 7770 Überlingen Geschwindigkeitsregler fuer flugzeuge
US3547501A (en) * 1969-12-12 1970-12-15 Gen Motors Corp Antilock brake control
US3624364A (en) * 1970-01-28 1971-11-30 Us Army Parallel speed stabilization system

Also Published As

Publication number Publication date
FR2139096A1 (member.php) 1973-01-05
CA973953A (en) 1975-09-02
GB1340448A (en) 1973-12-12
IT959696B (it) 1973-11-10
DE2223975A1 (de) 1973-02-15
FR2139096B1 (member.php) 1977-12-23
US3724786A (en) 1973-04-03

Similar Documents

Publication Publication Date Title
DE69217229T2 (de) System zur vertikalen steuerung für drehflügelflugzeug
DE2904800C2 (de) Flugzeug-uebersinkfluggeschwindigkeit- warnanordnung
DE69210193T2 (de) Methode und Vorrichtung zur Regelung des Schubes eines Flugzeuges während des Steigfluges
DE1263146C2 (de) Selbstanpassendes Regelsystem
DE3881667T2 (de) Steuerungssystem für Hubschrauber.
DE3884745T2 (de) Vorrichtung zur steuerung der geschwindigkeit eines servomotors.
DE3407247C2 (de) Automatische, drehmomentbegrenzende Flughöhenregelanlage für einen Hubschrauber
CH654536A5 (de) Anordnung zum erzeugen eines fluggeschwindigkeitssignals.
DE2530305C2 (de) Brennstoffregeleinrichtung für Gasturbinentriebwerke
DE68920991T2 (de) Flugkontrollsystem für Nicklagensteuerung zum Abfangen vor der Landung.
DE3729963A1 (de) Antiblockierbremsregelsystem mit fahrgeschwindigkeitsabhaengigem schlupfgrenzwert
DE3787741T2 (de) Verfahren und Gerät zur Steuerung eines Flugzeuges im Bereich der Windscherung.
DE2936696A1 (de) Geschwindigkeitsregelanordnung fuer flugzeuge
DE69534781T2 (de) Verfahren zur Erzeugung eines Seitenrudersteuerbefehls zur Kompensation eines unsymmetrischen Schubs für ein Flugzeug
DE69532632T2 (de) Flugzeug-Regelsystem für vertikale Position
DE2223975B2 (de) Regelvorrichtung fur die Grundgeschwindigkeit eines Hubschraubers
DE69119325T2 (de) Verfahren und Vorrichtung zur Überwachung des gesteuerten Befehls für ein Flugzeug mit Begrenzung von einem vorbestimmten Flugparameter
DE1481549B2 (de) Geschwindigkeitsregler fuer flugzeuge
DE1531549C3 (de) Druckregeleinrichtung für Flugzeugkabinen
DE69022880T2 (de) Hubschraubersteuerung mit mehreren Programmen für die Vorhersage des Abklingens der Rotorgeschwindigkeit.
DE3429721A1 (de) Verfahren und einrichtung fuer aufzug-gleichstrom-antriebsmotor-stabilisierung
DE60304533T2 (de) Verfahren und Einrichtung zur automatischen Steuerung des Schubes eines Flugzeugantriebes
DE69504497T2 (de) Verfahren zur Unterdrückung eines koordinierten Kursabweichungssystems in einem Regelungssystem für Hubschrauber
DE69304329T2 (de) Steuerungssystem zum koordinieren des umlenkens oder des beibehaltens des kurswinkels eines hubschraubers
DE2139452A1 (de) Automatisches Flugsteuerungssystem für Luftfahrzeuge

Legal Events

Date Code Title Description
8239 Disposal/non-payment of the annual fee