FR2730303B1 - Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvre - Google Patents

Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvre

Info

Publication number
FR2730303B1
FR2730303B1 FR9601289A FR9601289A FR2730303B1 FR 2730303 B1 FR2730303 B1 FR 2730303B1 FR 9601289 A FR9601289 A FR 9601289A FR 9601289 A FR9601289 A FR 9601289A FR 2730303 B1 FR2730303 B1 FR 2730303B1
Authority
FR
France
Prior art keywords
missile
implementing
vehicle
movement
machine
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
FR9601289A
Other languages
English (en)
Other versions
FR2730303A1 (fr
Inventor
Wayne K Schroeder
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
Loral Vought Systems 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 Loral Vought Systems Corp filed Critical Loral Vought Systems Corp
Publication of FR2730303A1 publication Critical patent/FR2730303A1/fr
Application granted granted Critical
Publication of FR2730303B1 publication Critical patent/FR2730303B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR9601289A 1995-02-03 1996-02-02 Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvre Expired - Fee Related FR2730303B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/383,720 US5631830A (en) 1995-02-03 1995-02-03 Dual-control scheme for improved missle maneuverability

Publications (2)

Publication Number Publication Date
FR2730303A1 FR2730303A1 (fr) 1996-08-09
FR2730303B1 true FR2730303B1 (fr) 2000-02-11

Family

ID=23514416

Family Applications (2)

Application Number Title Priority Date Filing Date
FR9601289A Expired - Fee Related FR2730303B1 (fr) 1995-02-03 1996-02-02 Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvre
FR9908299A Withdrawn FR2779246A1 (fr) 1995-02-03 1999-06-29 Procede et systeme pour changer rapidement la direction de deplacement d'un vehicule se deplacant dans un milieu fluide

Family Applications After (1)

Application Number Title Priority Date Filing Date
FR9908299A Withdrawn FR2779246A1 (fr) 1995-02-03 1999-06-29 Procede et systeme pour changer rapidement la direction de deplacement d'un vehicule se deplacant dans un milieu fluide

Country Status (3)

Country Link
US (3) US5631830A (fr)
DE (1) DE19603771A1 (fr)
FR (2) FR2730303B1 (fr)

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US7624941B1 (en) * 2006-05-02 2009-12-01 Orbital Research Inc. Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators
US8546736B2 (en) 2007-03-15 2013-10-01 Raytheon Company Modular guided projectile
US7947938B2 (en) * 2007-03-15 2011-05-24 Raytheon Company Methods and apparatus for projectile guidance
US8436283B1 (en) 2008-07-11 2013-05-07 Davidson Technologies Inc. System and method for guiding and controlling a missile using high order sliding mode control
US8173946B1 (en) 2008-08-26 2012-05-08 Raytheon Company Method of intercepting incoming projectile
US9170070B2 (en) 2012-03-02 2015-10-27 Orbital Atk, Inc. Methods and apparatuses for active protection from aerial threats
US9551552B2 (en) 2012-03-02 2017-01-24 Orbital Atk, Inc. Methods and apparatuses for aerial interception of aerial threats
US9501055B2 (en) 2012-03-02 2016-11-22 Orbital Atk, Inc. Methods and apparatuses for engagement management of aerial threats
US11947349B2 (en) 2012-03-02 2024-04-02 Northrop Grumman Systems Corporation Methods and apparatuses for engagement management of aerial threats
US11313650B2 (en) 2012-03-02 2022-04-26 Northrop Grumman Systems Corporation Methods and apparatuses for aerial interception of aerial threats
RU2512047C1 (ru) * 2012-11-29 2014-04-10 Открытое акционерное общество "Конструкторское бюро приборостроения" Управляемая пуля
US9121680B2 (en) 2013-01-17 2015-09-01 Raytheon Company Air vehicle with control surfaces and vectored thrust
US9068808B2 (en) 2013-01-17 2015-06-30 Raytheon Company Air vehicle with bilateral steering thrusters
DE102014004251A1 (de) * 2013-11-20 2015-06-25 Mbda Deutschland Gmbh Lenkflugkörper und Verfahren zum Lenken eines Lenkflugkörpers
CN104019701B (zh) * 2014-05-28 2016-07-06 中国人民解放军海军航空工程学院 一种利用直接力气动力复合控制的前向拦截制导方法
US10113844B1 (en) 2016-11-21 2018-10-30 Lockheed Martin Corporation Missile, chemical plasm steering system, and method
US10914559B1 (en) 2016-11-21 2021-02-09 Lockheed Martin Corporation Missile, slot thrust attitude controller system, and method
CN108168381B (zh) * 2018-01-04 2019-10-08 北京理工大学 一种多枚导弹协同作战的控制方法
CN114417730B (zh) * 2022-01-27 2022-09-16 哈尔滨逐宇航天科技有限责任公司 基于集成神经网络的飞行器滑翔段飞行范围在线预示方法
DE102022001289A1 (de) * 2022-04-13 2023-10-19 Diehl Defence Gmbh & Co. Kg Verfahren zum Ausweichen eines Flugkörpers vor einem Abfangflugkörper

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Also Published As

Publication number Publication date
FR2730303A1 (fr) 1996-08-09
FR2779246A1 (fr) 1999-12-03
US5835869A (en) 1998-11-10
DE19603771A1 (de) 1996-08-08
US5631830A (en) 1997-05-20
USRE37331E1 (en) 2001-08-14

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CD Change of name or company name
TP Transmission of property
ST Notification of lapse

Effective date: 20131031