CA1081828A - Stability augmentation systems - Google Patents

Stability augmentation systems

Info

Publication number
CA1081828A
CA1081828A CA270,579A CA270579A CA1081828A CA 1081828 A CA1081828 A CA 1081828A CA 270579 A CA270579 A CA 270579A CA 1081828 A CA1081828 A CA 1081828A
Authority
CA
Canada
Prior art keywords
aircraft
comparator
signal
actual
signals
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
CA270,579A
Other languages
English (en)
French (fr)
Inventor
Joseph R. Maciolek
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
Application granted granted Critical
Publication of CA1081828A publication Critical patent/CA1081828A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of 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)
  • Navigation (AREA)
CA270,579A 1976-04-12 1977-01-27 Stability augmentation systems Expired CA1081828A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US05/675,707 US4032083A (en) 1976-04-12 1976-04-12 Automatic gain control for stability augmentation systems
US675,707 1976-04-12

Publications (1)

Publication Number Publication Date
CA1081828A true CA1081828A (en) 1980-07-15

Family

ID=24711644

Family Applications (1)

Application Number Title Priority Date Filing Date
CA270,579A Expired CA1081828A (en) 1976-04-12 1977-01-27 Stability augmentation systems

Country Status (8)

Country Link
US (1) US4032083A (OSRAM)
JP (1) JPS52126900A (OSRAM)
CA (1) CA1081828A (OSRAM)
DE (1) DE2715690A1 (OSRAM)
FR (1) FR2348104A1 (OSRAM)
GB (1) GB1538968A (OSRAM)
IL (1) IL51714A (OSRAM)
IT (1) IT1076144B (OSRAM)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4115755A (en) * 1976-06-11 1978-09-19 United Technologies Corporation Aerodynamic surface load sensing
US4304375A (en) * 1979-05-17 1981-12-08 Textron Inc. Electrically controlled elevator
US4312042A (en) * 1979-12-12 1982-01-19 Sundstrand Data Control, Inc. Weight, balance, and tire pressure detection systems
US4312039A (en) * 1980-01-24 1982-01-19 Sperry Corporation Transient free synchronization system
US4545019A (en) * 1982-06-18 1985-10-01 Sundstrand Corporation Aircraft in-flight center of gravity measuring system
US5971325A (en) * 1997-12-23 1999-10-26 Sikorsky Aircraft Corporation Compensation for rotorcraft pitch axis control saturation
US7762501B2 (en) 2005-08-31 2010-07-27 Bell Helicopter Textron Inc. Method and apparatus for improving main rotor yoke fatigue life
US7742846B2 (en) * 2006-06-02 2010-06-22 Sikorsky Aircraft Corporation Surface contact override landing scheme for a FBW rotary-wing aircraft

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA624266A (en) * 1961-07-25 Kolisch Emil Center of gravity equipment for aircraft
US3071335A (en) * 1958-10-03 1963-01-01 United Aircraft Corp Flight control system
US3194058A (en) * 1962-09-18 1965-07-13 Kurkjian Haig Weight and balance determination
FR1353123A (fr) * 1963-02-13 1964-02-21 North American Aviation Inc Système de commande de vol automatique pour hélicoptère
US3616691A (en) * 1969-03-26 1971-11-02 Bendix Corp Mission capability indicating system
US3701279A (en) * 1971-02-08 1972-10-31 Electro Dev Corp Aircraft weight and center of gravity indicator system

Also Published As

Publication number Publication date
GB1538968A (en) 1979-01-24
IT1076144B (it) 1985-04-24
FR2348104A1 (fr) 1977-11-10
JPS52126900A (en) 1977-10-25
IL51714A (en) 1981-07-31
DE2715690A1 (de) 1977-10-20
FR2348104B1 (OSRAM) 1982-07-23
US4032083A (en) 1977-06-28

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Legal Events

Date Code Title Description
MKEX Expiry