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DE69315444D1 - Vorrichtung zur nutationsdämpfung für kreisel - Google Patents

Vorrichtung zur nutationsdämpfung für kreisel

Info

Publication number
DE69315444D1
DE69315444D1 DE69315444T DE69315444T DE69315444D1 DE 69315444 D1 DE69315444 D1 DE 69315444D1 DE 69315444 T DE69315444 T DE 69315444T DE 69315444 T DE69315444 T DE 69315444T DE 69315444 D1 DE69315444 D1 DE 69315444D1
Authority
DE
Germany
Prior art keywords
gyros
nutation damping
nutation
damping
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 - Fee Related
Application number
DE69315444T
Other languages
English (en)
Other versions
DE69315444T2 (de
Inventor
David Amberntson
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.)
Lockheed Martin Corp
Original Assignee
Martin Marietta 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 Martin Marietta Corp filed Critical Martin Marietta Corp
Publication of DE69315444D1 publication Critical patent/DE69315444D1/de
Application granted granted Critical
Publication of DE69315444T2 publication Critical patent/DE69315444T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/222—Homing guidance systems for spin-stabilized missiles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/366—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using magnetometers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2213—Homing guidance systems maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/12—Gyroscopes
    • Y10T74/1229—Gyroscope control
    • Y10T74/1257—Damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Engineering (AREA)
  • Vibration Prevention Devices (AREA)
DE69315444T 1992-12-22 1993-12-20 Vorrichtung zur nutationsdämpfung für kreisel Expired - Fee Related DE69315444T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/995,080 US5315888A (en) 1992-12-22 1992-12-22 Gyro nutation damper
PCT/US1993/012410 WO1994014654A1 (en) 1992-12-22 1993-12-20 Gyro nutation damper

Publications (2)

Publication Number Publication Date
DE69315444D1 true DE69315444D1 (de) 1998-01-08
DE69315444T2 DE69315444T2 (de) 1998-03-19

Family

ID=25541366

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69315444T Expired - Fee Related DE69315444T2 (de) 1992-12-22 1993-12-20 Vorrichtung zur nutationsdämpfung für kreisel

Country Status (4)

Country Link
US (1) US5315888A (de)
EP (1) EP0675825B1 (de)
DE (1) DE69315444T2 (de)
WO (1) WO1994014654A1 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5820079A (en) * 1994-04-05 1998-10-13 Hughes Electronics Mechanism for mounting and actuating a momentum wheel with high vibration isolation
FR2873436B1 (fr) * 2004-07-20 2006-11-17 Sagem Systeme embarque de guidage d'un projectile et projectile equipe d'un tel systeme
US7862056B2 (en) * 2007-02-02 2011-01-04 Ford Global Technologies, Llc Steering gear inertia damper
US20120096984A1 (en) * 2009-07-08 2012-04-26 Bill Gray Flywheel System

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2226902A (en) * 1938-04-14 1940-12-31 Siemens App Und Maschinen Gmbh Damping means for indicating instruments
US2534963A (en) * 1948-05-03 1950-12-19 Gen Electric Nutation damper for gyroscopes
US3480232A (en) * 1965-11-22 1969-11-25 Us Navy Damping coupler for satellite attitude control
US3426980A (en) * 1966-01-05 1969-02-11 Gen Electric Double tuned nutation damper
US3442468A (en) * 1966-11-14 1969-05-06 Hughes Aircraft Co Nutation damped stabilized device
US3523458A (en) * 1967-11-13 1970-08-11 Sanders Associates Inc Damping means for rate gyros
US3877316A (en) * 1971-06-09 1975-04-15 Hughes Aircraft Co Isolated frame on platform stabilized by spinning body
GB1570529A (en) * 1976-07-02 1980-07-02 British Aircraft Corp Ltd Nutation neutralising devices for spacecraft
JPS5927215A (ja) * 1982-08-06 1984-02-13 Furuno Electric Co Ltd ジヤイロコンパスにおける短期静定装置

Also Published As

Publication number Publication date
US5315888A (en) 1994-05-31
WO1994014654A1 (en) 1994-07-07
EP0675825A1 (de) 1995-10-11
EP0675825B1 (de) 1997-11-26
DE69315444T2 (de) 1998-03-19

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee