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IT8249227A0 - Procedimento ed apparecchio per il pilotaggio di un corpo aerodinamico dotato di radioguida - Google Patents

Procedimento ed apparecchio per il pilotaggio di un corpo aerodinamico dotato di radioguida

Info

Publication number
IT8249227A0
IT8249227A0 IT8249227A IT4922782A IT8249227A0 IT 8249227 A0 IT8249227 A0 IT 8249227A0 IT 8249227 A IT8249227 A IT 8249227A IT 4922782 A IT4922782 A IT 4922782A IT 8249227 A0 IT8249227 A0 IT 8249227A0
Authority
IT
Italy
Prior art keywords
piloting
procedure
equipment
body equipped
aerodynamic body
Prior art date
Application number
IT8249227A
Other languages
English (en)
Other versions
IT1203644B (it
Inventor
Bengt Skarman
Original Assignee
Saab Scania Ab
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 Saab Scania Ab filed Critical Saab Scania Ab
Publication of IT8249227A0 publication Critical patent/IT8249227A0/it
Application granted granted Critical
Publication of IT1203644B publication Critical patent/IT1203644B/it

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Power Steering Mechanism (AREA)
  • Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)
  • Feedback Control In General (AREA)
IT49227/82A 1981-10-08 1982-10-07 Procedimento ed apparecchio per il pilotaggio di un corpo aerodinamico dotato di radioguida IT1203644B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE8105948A SE430102B (sv) 1981-10-08 1981-10-08 Sett och anordning for styrning av en aerodynamisk kropp med skrovfast malsokare

Publications (2)

Publication Number Publication Date
IT8249227A0 true IT8249227A0 (it) 1982-10-07
IT1203644B IT1203644B (it) 1989-02-15

Family

ID=20344729

Family Applications (1)

Application Number Title Priority Date Filing Date
IT49227/82A IT1203644B (it) 1981-10-08 1982-10-07 Procedimento ed apparecchio per il pilotaggio di un corpo aerodinamico dotato di radioguida

Country Status (12)

Country Link
US (1) US4529151A (it)
EP (1) EP0100319B1 (it)
JP (1) JPS58501688A (it)
AU (1) AU549393B2 (it)
CA (1) CA1196420A (it)
DE (1) DE3275314D1 (it)
DK (1) DK149724C (it)
FI (1) FI73828C (it)
IT (1) IT1203644B (it)
SE (1) SE430102B (it)
WO (1) WO1983001298A1 (it)
YU (2) YU45119B (it)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111913491A (zh) * 2020-09-22 2020-11-10 中国人民解放军海军航空大学 一种基于视线角非线性抗饱和与不确定性补偿的制导方法

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0222571A3 (en) * 1985-10-31 1988-05-04 British Aerospace Public Limited Company Line of sight missile guidance
US5022608A (en) * 1990-01-08 1991-06-11 Hughes Aircraft Company Lightweight missile guidance system
US5064141A (en) * 1990-02-16 1991-11-12 Raytheon Company Combined sensor guidance system
RU2021577C1 (ru) * 1992-06-30 1994-10-15 Машиностроительное Конструкторское Бюро "Факел" Способ управления снарядом
CA2161045A1 (en) * 1994-11-15 1996-05-16 Michael L. Wells Error detector apparatus with digital coordinate transformation
US5975460A (en) * 1997-11-10 1999-11-02 Raytheon Company Nonlinear guidance gain factor for guided missiles
WO2001087590A1 (fr) 2000-05-19 2001-11-22 Tdk Corporation Film fonctionnel avec couche fonctionnelle et article dote d'un tel film
US8288696B1 (en) * 2007-07-26 2012-10-16 Lockheed Martin Corporation Inertial boost thrust vector control interceptor guidance
US7795565B2 (en) * 2008-01-03 2010-09-14 Lockheed Martin Corporation Guidance system with varying error correction gain
US8946606B1 (en) * 2008-03-26 2015-02-03 Arete Associates Determining angular rate for line-of-sight to a moving object, with a body-fixed imaging sensor

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3181813A (en) * 1956-08-10 1965-05-04 Jr Joseph F Gulick Inter-ferometer homing system
FR1265834A (fr) * 1959-03-31 1961-07-07 Sud Aviation Procédé et dispositif d'auto-guidage d'un engin sur une cible mobile
DE1174655B (de) * 1961-02-18 1964-07-23 Messerschmitt Ag Verfahren zur Lenkung eines Traegers von Geschossen auf der Ortskurve ballistischer Schusspositionen und Einrichtung zur Aus-fuehrung des Verfahrens
US3372890A (en) * 1966-02-04 1968-03-12 Martin Marietta Corp Data processor for circular scanning tracking system
US3523659A (en) * 1968-03-04 1970-08-11 Gen Dynamics Corp Rolling missile guidance system having body fixed antennas
CA1009370A (en) * 1972-01-03 1977-04-26 Ship Systems Laser guided projectile
JPS552555B2 (it) * 1972-09-28 1980-01-21
US4037202A (en) * 1975-04-21 1977-07-19 Raytheon Company Microprogram controlled digital processor having addressable flip/flop section
US4168813A (en) * 1976-10-12 1979-09-25 The Boeing Company Guidance system for missiles
DE2738507C3 (de) * 1977-08-26 1980-08-07 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Verfahren zur Erhöhung der Treffwahrscheinlichkeit von gestörten Flugkörpern und Einrichtung zur Durchführung des Verfahrens
DE2830502C3 (de) * 1978-07-12 1981-10-08 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Steuervorrichtung für Flugkörper
FR2474686B1 (fr) * 1980-01-29 1986-04-04 Europ Propulsion Systeme d'auto-guidage simplifie pour engin du type obus ou roquette
US4456862A (en) * 1982-09-22 1984-06-26 General Dynamics, Pomona Division Augmented proportional navigation in second order predictive scheme

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111913491A (zh) * 2020-09-22 2020-11-10 中国人民解放军海军航空大学 一种基于视线角非线性抗饱和与不确定性补偿的制导方法

Also Published As

Publication number Publication date
SE430102B (sv) 1983-10-17
EP0100319A1 (en) 1984-02-15
DK149724B (da) 1986-09-15
YU45119B (en) 1992-03-10
FI834081A (fi) 1983-11-08
DK256083D0 (da) 1983-06-06
YU108286A (en) 1988-12-31
FI73828B (fi) 1987-07-31
FI73828C (fi) 1987-11-09
AU549393B2 (en) 1986-01-23
JPS58501688A (ja) 1983-10-06
YU46693B (sh) 1994-04-05
AU8996582A (en) 1983-04-27
WO1983001298A1 (en) 1983-04-14
SE8105948L (sv) 1983-04-09
IT1203644B (it) 1989-02-15
EP0100319B1 (en) 1987-01-28
CA1196420A (en) 1985-11-05
YU227882A (en) 1990-06-30
FI834081A0 (fi) 1983-11-08
DE3275314D1 (en) 1987-03-05
US4529151A (en) 1985-07-16
DK256083A (da) 1983-06-06
DK149724C (da) 1987-04-06

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19971030