GB1170596A - Devices for use in Stabilising the Attitude of a Body - Google Patents

Devices for use in Stabilising the Attitude of a Body

Info

Publication number
GB1170596A
GB1170596A GB41465/66A GB4146566A GB1170596A GB 1170596 A GB1170596 A GB 1170596A GB 41465/66 A GB41465/66 A GB 41465/66A GB 4146566 A GB4146566 A GB 4146566A GB 1170596 A GB1170596 A GB 1170596A
Authority
GB
United Kingdom
Prior art keywords
attitude
demodulator
output
ship
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
GB41465/66A
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.)
FILOTECNICA SALMOIRAGHI SpA
Original Assignee
FILOTECNICA SALMOIRAGHI SpA
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 FILOTECNICA SALMOIRAGHI SpA filed Critical FILOTECNICA SALMOIRAGHI SpA
Publication of GB1170596A publication Critical patent/GB1170596A/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
    • G05D1/0875Control of attitude, i.e. control of roll, pitch, or yaw specially adapted to water vehicles
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)

Abstract

1,170,596. Electric correspondence control systems. FILOTECNICA SALMOIRAGHI S.p.A. Sept.16, 1966 [Nov. 19, 1965], No.41465/66. Heading G1N. The attitude of a body mounted on a body carrying a gyroscope is automatically stabilized by electric signals from the gyro. As applied to stabilizing the attitude of an instrument mounted on a ship an attitude gyro g Fig. 1, on the ship produces an alternating voltage giving an indication of roll amplitude, frequency and mean list of the ship. This voltage, after amplification at a, is applied to a demodulator c which also receives a reference voltage from an amplifier b. The direct voltage output of demodulator c is applied through an amplifier d and biased diode limiter e to produce an output which is utilized to stabilize the instrument. To eliminate drift, the limited output signal is also applied through an integratoramplifier f as negative feedback for combination with the output of demodulator c. Suitable transistor circuits are outlined.
GB41465/66A 1965-11-19 1966-09-16 Devices for use in Stabilising the Attitude of a Body Expired GB1170596A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT2576965 1965-11-19

Publications (1)

Publication Number Publication Date
GB1170596A true GB1170596A (en) 1969-11-12

Family

ID=11217672

Family Applications (1)

Application Number Title Priority Date Filing Date
GB41465/66A Expired GB1170596A (en) 1965-11-19 1966-09-16 Devices for use in Stabilising the Attitude of a Body

Country Status (2)

Country Link
FR (1) FR1500305A (en)
GB (1) GB1170596A (en)

Also Published As

Publication number Publication date
FR1500305A (en) 1967-11-03

Similar Documents

Publication Publication Date Title
GB1019088A (en) Turbine control system
GB1479120A (en) Aircraft ground proximity warming system
GB1340293A (en) Load stability system
GB1038325A (en) Controlled amplitude oscillator
GB1093549A (en) Gyroscopic inertial instruments and guidance systems
GB1485905A (en) Gain control circuit
GB940853A (en) Voltage sensitive regulating or control circuit
GB994999A (en) Servo systems
GB1170596A (en) Devices for use in Stabilising the Attitude of a Body
GB1187145A (en) Improved Vehicle Presence Detector System.
GB1149435A (en) Method of homing and guiding flying bodies
GB1070211A (en) Improvements relating to stability augmentation systems for craft
GB1210373A (en) Improvements in or relating to ships' roll stabilizer control systems
GB706494A (en) Improvements in or relating to gyro-verticals
GB947260A (en) Improvements in or relating to alternating current generators
GB970454A (en) Improvements in demodulators
GB952223A (en) Improvements in or relating to multi-signal common channel amplifiers
SU136906A1 (en) Integrator on a magnetic amplifier
GB1233168A (en)
MATYTSIN Aircraft stability and method for determining optimum parameters of static and nonstatic autopilots
GB1088482A (en) Improvements in or relating to inverters
GB863457A (en) Vertical reference-defining apparatus
KR830009703A (en) Signal extender
GB863458A (en) Craft navigation systems
CHAPMAN Analysis of guidance system errors resulting from initial misalignments of both the accelerometer and stabilizing gyros, the drift of the stabilized element during flight and errors in measuring the vehicle motions