DE1431190B2 - - Google Patents

Info

Publication number
DE1431190B2
DE1431190B2 DE19641431190 DE1431190A DE1431190B2 DE 1431190 B2 DE1431190 B2 DE 1431190B2 DE 19641431190 DE19641431190 DE 19641431190 DE 1431190 A DE1431190 A DE 1431190A DE 1431190 B2 DE1431190 B2 DE 1431190B2
Authority
DE
Germany
Prior art keywords
voltage
capacitor
circuit
threshold value
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
DE19641431190
Other languages
German (de)
English (en)
Other versions
DE1431190A1 (de
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 filed Critical
Publication of DE1431190A1 publication Critical patent/DE1431190A1/de
Publication of DE1431190B2 publication Critical patent/DE1431190B2/de
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • 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
    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
    • 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
    • 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

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)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Amplifiers (AREA)
DE19641431190 1963-05-31 1964-05-29 Stabilisierungssystem fuer Flugzeuge Pending DE1431190A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US284707A US3199013A (en) 1963-05-31 1963-05-31 Rate responsive compensation change circuit

Publications (2)

Publication Number Publication Date
DE1431190A1 DE1431190A1 (de) 1969-01-16
DE1431190B2 true DE1431190B2 (enFirst) 1970-10-29

Family

ID=23091221

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19641431190 Pending DE1431190A1 (de) 1963-05-31 1964-05-29 Stabilisierungssystem fuer Flugzeuge

Country Status (4)

Country Link
US (1) US3199013A (enFirst)
DE (1) DE1431190A1 (enFirst)
FR (1) FR1426125A (enFirst)
GB (1) GB1070211A (enFirst)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3949696A (en) * 1972-06-21 1976-04-13 Tokyo Keiki Company Limited Marine steering arrangement
US3908935A (en) * 1974-04-19 1975-09-30 Pneumo Dynamics Corp Aircraft duplex system
US4460858A (en) * 1982-05-11 1984-07-17 The Boeing Company Autopilot roll control wheel steering system
US4536689A (en) * 1984-05-17 1985-08-20 Sperry Corporation Servomotor feedback fault detector
JPH01248211A (ja) * 1988-03-29 1989-10-03 Teijin Seiki Co Ltd 安定性補償回路
US5079492A (en) * 1988-03-29 1992-01-07 Teijin Seiki Company Limited Stability compensating circuit

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2762962A (en) * 1950-06-21 1956-09-11 Smith & Sons Ltd S Safety device for automatic pilot system
US2973650A (en) * 1954-11-16 1961-03-07 Sperry Gyroscope Co Ltd Safety device for control systems for aircraft

Also Published As

Publication number Publication date
DE1431190A1 (de) 1969-01-16
GB1070211A (en) 1967-06-01
US3199013A (en) 1965-08-03
FR1426125A (fr) 1966-01-28

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Legal Events

Date Code Title Description
E77 Valid patent as to the heymanns-index 1977