DE3210817C2 - - Google Patents

Info

Publication number
DE3210817C2
DE3210817C2 DE3210817A DE3210817A DE3210817C2 DE 3210817 C2 DE3210817 C2 DE 3210817C2 DE 3210817 A DE3210817 A DE 3210817A DE 3210817 A DE3210817 A DE 3210817A DE 3210817 C2 DE3210817 C2 DE 3210817C2
Authority
DE
Germany
Prior art keywords
signal
attitude
line
pitch
airspeed
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
DE3210817A
Other languages
German (de)
English (en)
Other versions
DE3210817A1 (de
Inventor
Stuart Cammett Milford Conn. Us Wright
Don Luis Fairfield Conn. Us Adams
William Christian Monroe Conn. Us Fischer
David John Guilford Conn. Us Verzella
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 DE3210817A1 publication Critical patent/DE3210817A1/de
Application granted granted Critical
Publication of DE3210817C2 publication Critical patent/DE3210817C2/de
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
DE19823210817 1981-03-30 1982-03-24 System zum positionieren von die fluglage steuernden aerodynamischen flaechen eines flugzeuges Granted DE3210817A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/248,768 US4477876A (en) 1981-03-30 1981-03-30 Dual response aircraft reference synchronization

Publications (2)

Publication Number Publication Date
DE3210817A1 DE3210817A1 (de) 1982-10-21
DE3210817C2 true DE3210817C2 (enExample) 1992-02-06

Family

ID=22940600

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19823210817 Granted DE3210817A1 (de) 1981-03-30 1982-03-24 System zum positionieren von die fluglage steuernden aerodynamischen flaechen eines flugzeuges

Country Status (6)

Country Link
US (1) US4477876A (enExample)
JP (1) JPH0641278B2 (enExample)
BR (1) BR8201660A (enExample)
DE (1) DE3210817A1 (enExample)
GB (1) GB2095868B (enExample)
IT (1) IT1151380B (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5238203A (en) * 1991-08-28 1993-08-24 United Technologies Corporation High speed turn coordination for rotary wing aircraft
US5178307A (en) * 1991-08-28 1993-01-12 United Technologies Corporation High speed yaw control system for rotary wing aircraft
US5213283A (en) * 1991-08-28 1993-05-25 United Technologies Corporation Low speed turn coordination for rotary wing aircraft
US5169090A (en) * 1991-08-28 1992-12-08 United Technologies Corporation Attitude synchronization for model following control systems
US5222691A (en) * 1991-08-28 1993-06-29 United Technologies Corporation Automatic turn coordination trim control for rotary wing aircraft
FR2741855B1 (fr) * 1995-12-05 1998-01-30 Eurocopter France Systeme de manche cyclique assurant la stabilite en vitesse d'un helicoptere
US9157415B1 (en) * 2014-03-21 2015-10-13 General Electric Company System and method of controlling an electronic component of a wind turbine using contingency communications

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128968A (en) * 1964-04-14 Aircraft control servo apparatus having signal memorizing means
US2594326A (en) * 1947-12-31 1952-04-29 Bendix Aviat Corp Trim tab servomotor control
US3062486A (en) * 1958-11-19 1962-11-06 Honeywell Regulator Co Control system
US3275269A (en) * 1963-10-23 1966-09-27 Sperry Rand Corp Dual period aircraft control system
US3578268A (en) * 1969-01-21 1971-05-11 Lear Siegler Inc Automatic pitch control system
US3578269A (en) * 1969-06-11 1971-05-11 Lear Siegler Inc Automatic flare and altitude hold system
US4129275A (en) * 1974-11-22 1978-12-12 The Boeing Company Automatic flight control apparatus for aircraft
US4078749A (en) * 1977-05-24 1978-03-14 United Technologies Corporation Helicopter stick force augmentation null offset compensation
US4281811A (en) * 1979-06-15 1981-08-04 Edo-Aire Mitchell Pitch trim system for aircraft
US4382283A (en) * 1980-08-08 1983-05-03 United Technologies Corporation Helicopter attitude and airspeed acquisition and retention system

Also Published As

Publication number Publication date
GB2095868A (en) 1982-10-06
US4477876A (en) 1984-10-16
JPH0641278B2 (ja) 1994-06-01
IT8220488A0 (it) 1982-03-30
BR8201660A (pt) 1983-02-16
JPS5861098A (ja) 1983-04-11
IT1151380B (it) 1986-12-17
GB2095868B (en) 1984-08-30
DE3210817A1 (de) 1982-10-21

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Legal Events

Date Code Title Description
8128 New person/name/address of the agent

Representative=s name: MENGES, R., DIPL.-ING., PAT.-ANW., 8000 MUENCHEN

8110 Request for examination paragraph 44
8125 Change of the main classification

Ipc: G05D 1/08

D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee