GB1238765A - - Google Patents

Info

Publication number
GB1238765A
GB1238765A GB2402269A GB1238765DA GB1238765A GB 1238765 A GB1238765 A GB 1238765A GB 2402269 A GB2402269 A GB 2402269A GB 1238765D A GB1238765D A GB 1238765DA GB 1238765 A GB1238765 A GB 1238765A
Authority
GB
United Kingdom
Prior art keywords
plane
vector
angle
velocity
sight
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
GB2402269A
Other languages
English (en)
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 GB1238765A publication Critical patent/GB1238765A/en
Expired 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
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • 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
    • 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
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2286—Homing guidance systems characterised by the type of waves using radio waves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Radar Systems Or Details Thereof (AREA)
GB2402269A 1967-12-08 1969-05-12 Expired GB1238765A (https=)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE1531497 1967-12-08
GB2402269 1969-05-12

Publications (1)

Publication Number Publication Date
GB1238765A true GB1238765A (https=) 1971-07-07

Family

ID=25752716

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2402269A Expired GB1238765A (https=) 1967-12-08 1969-05-12

Country Status (2)

Country Link
US (1) US3603531A (https=)
GB (1) GB1238765A (https=)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4502650A (en) * 1982-09-22 1985-03-05 General Dynamics, Pomona Division Augmented proportional navigation in third order predictive scheme
US4456862A (en) * 1982-09-22 1984-06-26 General Dynamics, Pomona Division Augmented proportional navigation in second order predictive scheme
US4492352A (en) * 1982-09-22 1985-01-08 General Dynamics, Pomona Division Noise-adaptive, predictive proportional navigation (NAPPN) guidance scheme
US4494202A (en) * 1982-09-22 1985-01-15 General Dynamics, Pomona Division Fourth order predictive, augmented proportional navigation system terminal guidance design with missile/target decoupling
US5082200A (en) * 1990-12-03 1992-01-21 The United States Of America As Represented By The Secretary Of The Navy Method of guiding an in-flight vehicle toward a target
US5071087A (en) * 1991-03-11 1991-12-10 The United States Of America As Represented By The Secretary Of The Navy Method of guiding an in-flight vehicle to a desired flight path
US7513455B1 (en) * 2005-02-18 2009-04-07 Lockhead Martin Corporation Ballistic missile interceptor guidance by acceleration relative to line-of-sight
FR3030760B1 (fr) * 2014-12-18 2017-12-22 Airbus Helicopters Procede et systeme de determination d'une vitesse angulaire en virage pour un aeronef a voilure tournante

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2792190A (en) * 1951-02-28 1957-05-14 Helmut Ph G A R Von Zborowski Systems including a steerable vehicle and a finder device mounted thereon
US3028119A (en) * 1956-04-24 1962-04-03 Collins Radio Co Missile guidance system
GB1013150A (en) * 1958-12-01 1965-12-15 Dehavilland Aircraft A system for determining the parameters defining the relative motion of a moving object
CH401703A (de) * 1961-09-08 1965-10-31 Siemens Ag Albis Einrichtung zur selbsttätigen Regelung der Bewegung eines selbstgelenkten Flugkörpers nach einem Ziel
US3216614A (en) * 1963-05-07 1965-11-09 Symington Wayne Corp Coin operated dispensing apparatus

Also Published As

Publication number Publication date
US3603531A (en) 1971-09-07

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees