DE2343780C2 - Automatisches Flugsteuer- und -regelsystem für Bewegungen um die Hochachse oder Nickachse - Google Patents

Automatisches Flugsteuer- und -regelsystem für Bewegungen um die Hochachse oder Nickachse

Info

Publication number
DE2343780C2
DE2343780C2 DE2343780A DE2343780A DE2343780C2 DE 2343780 C2 DE2343780 C2 DE 2343780C2 DE 2343780 A DE2343780 A DE 2343780A DE 2343780 A DE2343780 A DE 2343780A DE 2343780 C2 DE2343780 C2 DE 2343780C2
Authority
DE
Germany
Prior art keywords
heading
devices
signal
output
voltage
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
DE2343780A
Other languages
German (de)
English (en)
Other versions
DE2343780A1 (de
Inventor
Ronald Eugene Phoenix Ariz. Thomas
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 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 Corp filed Critical Sperry Corp
Publication of DE2343780A1 publication Critical patent/DE2343780A1/de
Application granted granted Critical
Publication of DE2343780C2 publication Critical patent/DE2343780C2/de
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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
    • G05D1/0204—Control of position or course in two dimensions specially adapted to aircraft to counteract a sudden perturbation, e.g. cross-wind, gust
    • 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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to 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)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Gyroscopes (AREA)
  • Amplifiers (AREA)
DE2343780A 1972-08-30 1973-08-30 Automatisches Flugsteuer- und -regelsystem für Bewegungen um die Hochachse oder Nickachse Expired DE2343780C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00284781A US3848172A (en) 1972-08-30 1972-08-30 Yaw damper synchro system for aircraft

Publications (2)

Publication Number Publication Date
DE2343780A1 DE2343780A1 (de) 1974-03-21
DE2343780C2 true DE2343780C2 (de) 1982-12-09

Family

ID=23091510

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2343780A Expired DE2343780C2 (de) 1972-08-30 1973-08-30 Automatisches Flugsteuer- und -regelsystem für Bewegungen um die Hochachse oder Nickachse

Country Status (7)

Country Link
US (1) US3848172A (enExample)
JP (1) JPS4964200A (enExample)
CA (1) CA1003078A (enExample)
DE (1) DE2343780C2 (enExample)
FR (1) FR2198653A5 (enExample)
GB (1) GB1434076A (enExample)
IT (1) IT996119B (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4039165A (en) * 1976-06-04 1977-08-02 Sperry Rand Corporation Derived rate circuit for aircraft
US4084121A (en) * 1977-01-03 1978-04-11 General Electric Company Solid state repeater for three wire synchro with selectable phase and frequency adjustment
US4188570A (en) * 1978-07-28 1980-02-12 The United States Of America As Represented By The Secretary Of The Navy Gimbal angle rate feedback by cage coil demodulation
US4328483A (en) * 1980-02-01 1982-05-04 Sperry Corporation Multiplexed-demultiplexed synchro demodulation apparatus
US4626998A (en) * 1983-05-02 1986-12-02 United Technologies Corporation Heading reference trim system
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
EP0488428A3 (en) * 1990-09-24 1992-10-14 The Boeing Company Apparatus and method for reducing aircraft loads resulting from atmospheric turbulence and gusts
US5169090A (en) * 1991-08-28 1992-12-08 United Technologies Corporation Attitude synchronization for model following control systems
US5669582A (en) * 1995-05-12 1997-09-23 The Boeing Company Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to atmospheric turbulence and wind gusts
US6586901B1 (en) 2000-06-21 2003-07-01 Honeywell International Inc. Methods and apparatus suitable for facilitating control of an aircraft rudder

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB690670A (en) * 1950-06-14 1953-04-22 Sperry Corp Apparatus for damping oscillations of manually controlled dirigible craft
US3201669A (en) * 1960-04-08 1965-08-17 Dresser Ind Servo type integrator with means for minimizing the effects of friction
US3555391A (en) * 1966-03-11 1971-01-12 Thurman & Younkin Inc Open loop single axes servo flight control system
US3465256A (en) * 1967-05-16 1969-09-02 Honeywell Inc Shaft position indicator circuit for a synchro-transmitter
US3514719A (en) * 1967-06-21 1970-05-26 Collins Radio Co Electric analog angular rate deriving circuit
US3600694A (en) * 1970-04-27 1971-08-17 Collins Radio Co Power normalization of angular information from three-wire synchro source
US3710223A (en) * 1971-08-27 1973-01-09 North American Rockwell Position control system resolver
US3701936A (en) * 1971-12-10 1972-10-31 Collins Radio Co Fine & coarse synchro servomotor control including a dual sin/cosine to dc converter

Also Published As

Publication number Publication date
IT996119B (it) 1975-12-10
CA1003078A (en) 1977-01-04
FR2198653A5 (enExample) 1974-03-29
US3848172A (en) 1974-11-12
GB1434076A (en) 1976-04-28
JPS4964200A (enExample) 1974-06-21
DE2343780A1 (de) 1974-03-21

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Legal Events

Date Code Title Description
OHA Expiration of time for request for examination
8127 New person/name/address of the applicant

Owner name: SPERRY CORP., 10104 NEW YORK, N.Y., US

8180 Miscellaneous part 1

Free format text: WIEDEREINSETZUNG IN DEN VORHERGEHENDEN STAND

8110 Request for examination paragraph 44
D2 Grant after examination
8339 Ceased/non-payment of the annual fee