EP2405233A3 - Method for guiding a military missile - Google Patents

Method for guiding a military missile Download PDF

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Publication number
EP2405233A3
EP2405233A3 EP11005432.7A EP11005432A EP2405233A3 EP 2405233 A3 EP2405233 A3 EP 2405233A3 EP 11005432 A EP11005432 A EP 11005432A EP 2405233 A3 EP2405233 A3 EP 2405233A3
Authority
EP
European Patent Office
Prior art keywords
mission
data
type
mission component
component
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.)
Granted
Application number
EP11005432.7A
Other languages
German (de)
French (fr)
Other versions
EP2405233A2 (en
EP2405233B1 (en
Inventor
Thomas Dr. Kuhn
Wilhelm Hinding
Andreas Beutel
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.)
Diehl Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=44763678&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP2405233(A3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Publication of EP2405233A2 publication Critical patent/EP2405233A2/en
Publication of EP2405233A3 publication Critical patent/EP2405233A3/en
Application granted granted Critical
Publication of EP2405233B1 publication Critical patent/EP2405233B1/en
Revoked legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control
    • 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
    • F41G7/226—Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding 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
    • 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

Abstract

Die Erfindung geht aus von einem Verfahren zum Steuern eines Gefechtsflugkörpers (2), der einen Datenspeicher (24), ein Steuermittel (22) und eine Missionskomponente (50) enthält, bei dem das Steuermittel (22) die Missionskomponente (50) während eines Flugs des Gefechtsflugkörpers (2) steuert.The invention is directed to a method for controlling a combat missile (2) comprising a data memory (24), a control means (22) and a mission component (50), wherein the control means (22) controls the mission component (50) during a flight of the combat missile (2) controls.

Um eine Anpassung einer Flugkörpersteuerung an eine neue Missionskomponente (50) zu erleichtern, wird vorgeschlagen, dass der Datenspeicher (24) Erkennungsdaten zu einer Mehrzahl verschiedener Missionskomponenten (50) enthält und das Steuermittel (22) Typdaten aus der Missionskomponente (50) ausliest, den Typ der Missionskomponente (50) anhand der Erkennungsdaten und der Typdaten identifiziert und Steuerschritte in Abhängigkeit vom Typ der Missionskomponente (50) ausführt.

Figure imgaf001
In order to facilitate adaptation of a missile controller to a new mission component (50), it is proposed that the data memory (24) contains detection data for a plurality of different mission components (50) and the control means (22) reads type data from the mission component (50) Identifies the type of mission component (50) from the recognition data and the type data and performs control steps depending on the type of the mission component (50).
Figure imgaf001
EP11005432.7A 2010-07-08 2011-07-02 Method for guiding a military missile Revoked EP2405233B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010026428 2010-07-08
DE102010052202A DE102010052202A1 (en) 2010-07-08 2010-11-24 Method for controlling a combat missile

Publications (3)

Publication Number Publication Date
EP2405233A2 EP2405233A2 (en) 2012-01-11
EP2405233A3 true EP2405233A3 (en) 2014-06-25
EP2405233B1 EP2405233B1 (en) 2015-02-11

Family

ID=44763678

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11005432.7A Revoked EP2405233B1 (en) 2010-07-08 2011-07-02 Method for guiding a military missile

Country Status (3)

Country Link
EP (1) EP2405233B1 (en)
DE (1) DE102010052202A1 (en)
IL (1) IL213934A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015012970A1 (en) 2015-10-07 2017-04-13 Mbda Deutschland Gmbh Function-oriented and reconfigurable missile
DE102015013349B4 (en) * 2015-10-15 2023-05-17 Mbda Deutschland Gmbh Method of operating a weapon system
DE102017105565A1 (en) 2017-03-15 2018-09-20 Rheinmetall Waffe Munition Gmbh Ammunition and logistics concept for in particular artillery projectiles
CN112824820A (en) * 2019-11-21 2021-05-21 北京恒星箭翔科技有限公司 Reverse-low small slow target air defense missile system for 40 mm rocket launcher and intercepting method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2272047A (en) * 1989-12-14 1994-05-04 British Aerospace Missile
US20060272538A1 (en) * 2005-06-02 2006-12-07 Raytheon Company Multi-mode modular projectile
US7506587B1 (en) * 2007-02-20 2009-03-24 The United States Of Americas As Represented By The Secretary Of The Navy Modular projectile system

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2272047A (en) * 1989-12-14 1994-05-04 British Aerospace Missile
US20060272538A1 (en) * 2005-06-02 2006-12-07 Raytheon Company Multi-mode modular projectile
US7506587B1 (en) * 2007-02-20 2009-03-24 The United States Of Americas As Represented By The Secretary Of The Navy Modular projectile system

Also Published As

Publication number Publication date
IL213934A0 (en) 2011-12-01
IL213934A (en) 2014-12-31
DE102010052202A1 (en) 2012-01-12
EP2405233A2 (en) 2012-01-11
EP2405233B1 (en) 2015-02-11

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