DE2236794A1 - Steuersystem fuer mehrere hebeflugzeuge - Google Patents

Steuersystem fuer mehrere hebeflugzeuge

Info

Publication number
DE2236794A1
DE2236794A1 DE2236794A DE2236794A DE2236794A1 DE 2236794 A1 DE2236794 A1 DE 2236794A1 DE 2236794 A DE2236794 A DE 2236794A DE 2236794 A DE2236794 A DE 2236794A DE 2236794 A1 DE2236794 A1 DE 2236794A1
Authority
DE
Germany
Prior art keywords
aircraft
control
angle
load
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.)
Pending
Application number
DE2236794A
Other languages
German (de)
English (en)
Inventor
Joseph Richard Maciolek
John Joseph Wallace
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 Aircraft 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 Aircraft Corp filed Critical United Aircraft Corp
Publication of DE2236794A1 publication Critical patent/DE2236794A1/de
Pending 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying

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)
  • Tires In General (AREA)
  • Train Traffic Observation, Control, And Security (AREA)
DE2236794A 1971-08-02 1972-07-27 Steuersystem fuer mehrere hebeflugzeuge Pending DE2236794A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16821971A 1971-08-02 1971-08-02

Publications (1)

Publication Number Publication Date
DE2236794A1 true DE2236794A1 (de) 1973-02-22

Family

ID=22610593

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2236794A Pending DE2236794A1 (de) 1971-08-02 1972-07-27 Steuersystem fuer mehrere hebeflugzeuge

Country Status (6)

Country Link
US (1) US3746279A (OSRAM)
CA (1) CA956380A (OSRAM)
DE (1) DE2236794A1 (OSRAM)
FR (1) FR2148316B1 (OSRAM)
GB (1) GB1365429A (OSRAM)
IT (1) IT963657B (OSRAM)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4591112A (en) * 1975-09-09 1986-05-27 Piasecki Aircraft Corporation Vectored thrust airship
US7438259B1 (en) * 2006-08-16 2008-10-21 Piasecki Aircraft Corporation Compound aircraft control system and method
US8370003B2 (en) * 2008-05-27 2013-02-05 Wilfred So System and method for multiple aircraft lifting a common payload
US9043052B2 (en) 2008-05-27 2015-05-26 Wilfred So System and method for multiple vehicles moving a common payload
US9829344B2 (en) * 2015-03-18 2017-11-28 The Boeing Company Cable angle sensor
US10318903B2 (en) 2016-05-06 2019-06-11 General Electric Company Constrained cash computing system to optimally schedule aircraft repair capacity with closed loop dynamic physical state and asset utilization attainment control
US12174642B2 (en) * 2016-06-21 2024-12-24 Keith Guy Modular robotic system
US10180687B2 (en) * 2016-07-27 2019-01-15 Kitty Hawk Corporation Maintaining a stable phase difference between multiple tethered vehicles lifting a payload
US12216480B2 (en) * 2020-05-01 2025-02-04 United States Of America, As Represented By The Secretary Of The Army Aircraft multi-lift system with synchronized maneuvering and load feedback control
US20250021111A1 (en) * 2021-12-04 2025-01-16 Uavpatent Corp. Coordinated drone operation

Also Published As

Publication number Publication date
US3746279A (en) 1973-07-17
FR2148316A1 (OSRAM) 1973-03-16
GB1365429A (en) 1974-09-04
CA956380A (en) 1974-10-15
IT963657B (it) 1974-01-21
FR2148316B1 (OSRAM) 1976-05-21

Similar Documents

Publication Publication Date Title
DE3877066T2 (de) Roll- und giersteuerungssystem fuer ein luftfahrzeug.
DE3111604C2 (OSRAM)
DE2233938C3 (de) Einrichtung zur Steuerung eines Drehflügelflugzeuges
DE2310045A1 (de) Flugsteuereinrichtung fuer senkrechtoder kurzstartende luftfahrzeuge
DE19914445B4 (de) Steuereinrichtung für einen beweglichen Körper
DE202010002309U1 (de) Reglereinrichtung für Helikopter
DE2161401A1 (de) Steuerungs- und Regelvorrichtung für Luftfahrzeuge
DE102018100332B4 (de) Mehrkörperflugzeug und Verfahren zur Regelung der Gesamtformation eines Mehrkörperflugzeugs
DE602005003679T2 (de) Elektrischer flugregler für flugzeughöhenruder
DE2808791C2 (OSRAM)
DE2236794A1 (de) Steuersystem fuer mehrere hebeflugzeuge
DE60025235T2 (de) System zur anpassung der steuerkraftgradienten eines steuerknüppels
DE69804859T2 (de) Kompensation für die steuerung der nickachse eines drehflüglers bei sättigung
DE1406491A1 (de) Flugsteuerungssystem fuer Hubschrauber
DE69510757T2 (de) Zyklisches Steuerungssystem mit Kraftgradientenrückführung für Hubschrauber
DE2236860A1 (de) Steuersystem fuer hebe- und transportvorgaenge mit mehreren flugzeugen
DE69502080T2 (de) Giersteuerung mit Kraftgradientenrückführung für Hubschrauber
DE102012106233B4 (de) Pendelanzeiger
DE2817323A1 (de) Hubschrauber und verfahren zum steuern desselben in kurven mit querneigung
DE1406448B2 (de) Regeleinrichtung zur stabilisierung der fluglage eines hubschraubers
DE1481548C3 (de) Vortriebsregler
DE102019130804B4 (de) Drohne, Verfahren zum Betreiben einer Drohne und Elektronische Steuer- und Regeleinrichtung zur Steuerung und Regelung des Betriebs einer Drohne
DE102015102459A1 (de) Verfahren und Vorrichtung zur Ansteuerung eines Simulators
DE2248453A1 (de) Ueberlastschutzvorrichtung fuer den rotor eines hubschraubers
DE69507168T2 (de) Stabilisierung eines funkgesteuerten luftfahrzeuges

Legal Events

Date Code Title Description
OHJ Non-payment of the annual fee