ITRM970718A1 - Complesso di guida per sistema di missile con dispositivo di inseguimento del bersaglio e supplementare correzione manuale del punto di aggancio. - Google Patents

Complesso di guida per sistema di missile con dispositivo di inseguimento del bersaglio e supplementare correzione manuale del punto di aggancio.

Info

Publication number
ITRM970718A1
ITRM970718A1 IT000718A ITRM970718A ITRM970718A1 IT RM970718 A1 ITRM970718 A1 IT RM970718A1 IT 000718 A IT000718 A IT 000718A IT RM970718 A ITRM970718 A IT RM970718A IT RM970718 A1 ITRM970718 A1 IT RM970718A1
Authority
IT
Italy
Prior art keywords
driving unit
tracking device
target tracking
manual correction
additional manual
Prior art date
Application number
IT000718A
Other languages
English (en)
Inventor
Richard Sturm
Original Assignee
Daimler Chrysler Aerospace Ag
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 Daimler Chrysler Aerospace Ag filed Critical Daimler Chrysler Aerospace Ag
Publication of ITRM970718A1 publication Critical patent/ITRM970718A1/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
    • 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
    • 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
    • F41G7/2206—Homing guidance systems using a remote control station
    • 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
    • F41G7/2253—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
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • 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
    • F41G7/24—Beam riding guidance systems
    • F41G7/26—Optical guidance 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
    • F41G7/30—Command link guidance 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
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • 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
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • F41G7/303—Sighting or tracking devices especially provided for simultaneous observation of the target and of the missile
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G9/00—Systems for controlling missiles or projectiles, not provided for elsewhere
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles
    • 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
    • G05D1/12—Target-seeking control

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Electromagnetism (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
IT000718A 1996-11-30 1997-11-21 Complesso di guida per sistema di missile con dispositivo di inseguimento del bersaglio e supplementare correzione manuale del punto di aggancio. ITRM970718A1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19649735A DE19649735A1 (de) 1996-11-30 1996-11-30 Lenkung für Flugkörper-Systeme mit Ziel-Tracker und zusätzlicher manueller Korrektur des Trackpunktes

Publications (1)

Publication Number Publication Date
ITRM970718A1 true ITRM970718A1 (it) 1999-05-21

Family

ID=33154645

Family Applications (1)

Application Number Title Priority Date Filing Date
IT000718A ITRM970718A1 (it) 1996-11-30 1997-11-21 Complesso di guida per sistema di missile con dispositivo di inseguimento del bersaglio e supplementare correzione manuale del punto di aggancio.

Country Status (5)

Country Link
US (1) US6808139B1 (it)
DE (1) DE19649735A1 (it)
FR (1) FR2885707B1 (it)
GB (3) GB9722585D0 (it)
IT (1) ITRM970718A1 (it)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101293247B1 (ko) * 2006-02-07 2013-08-09 삼성전자주식회사 자율 이동 로봇 및 그 제어 방법
US7566026B2 (en) * 2006-03-29 2009-07-28 Raytheon Company Onboard guidance method for ballistic missiles
US20090079837A1 (en) * 2007-09-24 2009-03-26 Honeywell International Inc. Image stabilization for image based navigation system
FR2936598B1 (fr) * 2008-09-30 2010-11-12 Mbda France Systeme de guidage d'un projectile
EP2209018A1 (en) * 2009-01-15 2010-07-21 Nederlandse Organisatie voor toegepast-natuurwetenschappelijk Onderzoek TNO A method for estimating an object motion characteristic from a radar signal, a computer system and a computer program product
CN103439977B (zh) * 2013-08-23 2016-03-02 西安应用光学研究所 适用于光电跟踪仪的高速目标跟踪控制方法
CN103533246B (zh) * 2013-10-22 2018-02-06 上海安奎拉信息技术有限公司 一种自动跟踪球形摄像机的控制方法
CN105159315B (zh) * 2015-09-01 2017-10-31 西北工业大学 面向空间绳系机器人的目标逼近过程鲁棒规划控制方法
CN108827302A (zh) * 2018-04-24 2018-11-16 大连理工大学 基于旋翼转速测量的多旋翼飞行器导航方法
CN111897223B (zh) * 2020-08-11 2021-04-20 哈尔滨工业大学 一种考虑自动驾驶仪动态特性的速度追踪制导方法
US11913757B2 (en) * 2022-01-18 2024-02-27 Rosemount Aerospace Inc. Constraining navigational drift in a munition

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1116801A (en) * 1963-03-22 1968-06-12 Dehavilland Aircraft Improvements in or relating to homing systems
US3742812A (en) * 1969-03-28 1973-07-03 Us Navy Method of aiming a television guided missile
US4027837A (en) * 1969-10-23 1977-06-07 The United States Of America As Represented By The Secretary Of The Army Optical tracking link utilizing pulse burst modulation for solid state missile beacons
US4047678A (en) * 1969-11-07 1977-09-13 The United States Of America As Represented By The Secretary Of The Army Modulated, dual frequency, optical tracking link for a command guidance missile system
GB1605342A (en) * 1969-11-13 1992-01-02 British Aerospace Improvements relating to missile guidance systems
US3876308A (en) * 1971-05-24 1975-04-08 Us Navy Automatic command guidance system using optical trackers
DE3543006A1 (de) * 1985-12-05 1989-11-02 Messerschmitt Boelkow Blohm Verfahren und einrichtung zum unterdruecken von stoerstrahlern im blickfeld eines bei der kommandolenkung von flugkoerpern eingesetzten ortungsgeraetes
GB8807355D0 (en) * 1988-03-28 2000-03-15 British Aerospace Missile guidance
US5626311A (en) * 1988-10-12 1997-05-06 Raytheon Company Method of guiding missiles
US5064141A (en) * 1990-02-16 1991-11-12 Raytheon Company Combined sensor guidance system
GB2285115A (en) * 1993-12-24 1995-06-28 Secr Defence Missile guiding system
DE4442134A1 (de) * 1994-11-26 1996-05-30 Bodenseewerk Geraetetech Lenkschleife für Flugkörper
JPH1163892A (ja) * 1997-08-19 1999-03-05 Mitsubishi Electric Corp 飛しょう体の誘導装置
US6181988B1 (en) * 1998-04-07 2001-01-30 Raytheon Company Guidance system having a body fixed seeker with an adjustable look angle

Also Published As

Publication number Publication date
GB2426601A (en) 2006-11-29
GB2432203B (en) 2011-01-12
GB2432203A (en) 2007-05-16
US6808139B1 (en) 2004-10-26
FR2885707A1 (fr) 2006-11-17
GB9725618D0 (en) 2006-02-15
GB0622814D0 (en) 2007-01-03
FR2885707B1 (fr) 2008-07-04
DE19649735A1 (de) 2007-06-06
GB9722585D0 (en) 2006-02-15
GB2426601B (en) 2007-05-02

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