EP4232771C0 - Abfangflugkörper und verfahren zu dessen lenkung - Google Patents

Abfangflugkörper und verfahren zu dessen lenkung

Info

Publication number
EP4232771C0
EP4232771C0 EP21791293.0A EP21791293A EP4232771C0 EP 4232771 C0 EP4232771 C0 EP 4232771C0 EP 21791293 A EP21791293 A EP 21791293A EP 4232771 C0 EP4232771 C0 EP 4232771C0
Authority
EP
European Patent Office
Prior art keywords
guiding
interceptor missile
interceptor
missile
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.)
Active
Application number
EP21791293.0A
Other languages
English (en)
French (fr)
Other versions
EP4232771A1 (de
EP4232771B1 (de
Inventor
Thomas Kuhn
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 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
Application filed by Diehl Defence GmbH and Co KG filed Critical Diehl Defence GmbH and Co KG
Publication of EP4232771A1 publication Critical patent/EP4232771A1/de
Application granted granted Critical
Publication of EP4232771C0 publication Critical patent/EP4232771C0/de
Publication of EP4232771B1 publication Critical patent/EP4232771B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F41G7/224—Deceiving or protecting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00—Defence installations; Defence devices
    • F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Power Steering Mechanism (AREA)
EP21791293.0A 2020-10-21 2021-10-08 Abfangflugkörper und verfahren zu dessen lenkung Active EP4232771B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102020006465.5A DE102020006465B4 (de) 2020-10-21 2020-10-21 Abfangflugkörper und Verfahren zu dessen Lenkung
PCT/EP2021/077884 WO2022084068A1 (de) 2020-10-21 2021-10-08 Abfangflugkörper und verfahren zu dessen lenkung

Publications (3)

Publication Number Publication Date
EP4232771A1 EP4232771A1 (de) 2023-08-30
EP4232771C0 true EP4232771C0 (de) 2024-09-11
EP4232771B1 EP4232771B1 (de) 2024-09-11

Family

ID=78179376

Family Applications (1)

Application Number Title Priority Date Filing Date
EP21791293.0A Active EP4232771B1 (de) 2020-10-21 2021-10-08 Abfangflugkörper und verfahren zu dessen lenkung

Country Status (7)

Country Link
US (1) US12228383B2 (de)
EP (1) EP4232771B1 (de)
KR (1) KR20230100722A (de)
AU (1) AU2021366148B2 (de)
DE (1) DE102020006465B4 (de)
IL (1) IL301348B2 (de)
WO (1) WO2022084068A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102022001289A1 (de) 2022-04-13 2023-10-19 Diehl Defence Gmbh & Co. Kg Verfahren zum Ausweichen eines Flugkörpers vor einem Abfangflugkörper
DE102022001285B4 (de) 2022-04-13 2024-08-22 Diehl Defence Gmbh & Co. Kg Verfahren zum Lenken eines Flugkörpers
DE102022001286A1 (de) 2022-04-13 2023-10-19 Diehl Defence Gmbh & Co. Kg Verfahren zur Midcourse-Lenkung eines im Schub steuerbaren Flugkörpers
CN114771877B (zh) * 2022-05-26 2022-11-18 哈尔滨工业大学 一种考虑导航误差的最优拦截制导方法
CN115129087B (zh) * 2022-07-26 2025-08-22 西北工业大学 基于滑翔飞行器目标机动能力分析和意图推断的拦截方法
CN116202373B (zh) * 2022-12-23 2025-01-17 中国人民解放军91892部队 一种无人机自主干扰拦截导弹方法
CN117647931B (zh) * 2023-12-18 2024-08-09 苏州星幕航天科技有限公司 一种惯性坐标系zem制导指令的等价最优性分析方法
CN118705942B (zh) * 2024-06-13 2025-11-04 北京航空航天大学 高超声速飞行器集群协同突防方法、设备、介质及产品
CN119558048B (zh) * 2024-11-12 2025-08-15 哈尔滨工业大学 一种多对一协同拦截快速弹道优化方法
KR102794244B1 (ko) * 2025-01-02 2025-04-15 (주)니어스랩 타겟 추적 장치 및 이의 제어 방법
CN120235229B (zh) * 2025-03-20 2025-11-25 北京控制工程研究所 一种在轨航天器广义智能控制系统架构及自主控制方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5435503A (en) * 1993-08-27 1995-07-25 Loral Vought Systems Corp. Real time missile guidance system
US5637826A (en) * 1996-02-07 1997-06-10 The United States Of America As Represented By The Secretary Of The Navy Method and apparatus for optimal guidance
DE10017600A1 (de) * 2000-04-08 2001-10-11 Bodenseewerk Geraetetech Regler, insbesondere Lenkregler für Flugkörper
US7513455B1 (en) * 2005-02-18 2009-04-07 Lockhead Martin Corporation Ballistic missile interceptor guidance by acceleration relative to line-of-sight
US7968831B2 (en) * 2007-06-12 2011-06-28 The Boeing Company Systems and methods for optimizing the aimpoint for a missile
US8106340B1 (en) 2009-03-02 2012-01-31 Lockheed Martin Corporation Generalized midcourse missile guidance
US8710411B1 (en) 2009-09-29 2014-04-29 Lockheed Martin Corporation Method and system for determining an optimal missile intercept approach direction for correct remote sensor-to-seeker handover
JP5577807B2 (ja) 2010-04-12 2014-08-27 三菱電機株式会社 飛しょう体誘導装置
DE102010032281A1 (de) 2010-07-26 2012-01-26 Diehl Bgt Defence Gmbh & Co. Kg Verfahren zum Steuern eines durch ein Triebwerk angetriebenen Lenkflugkörpers
EP2423774A1 (de) * 2010-08-23 2012-02-29 MBDA UK Limited Lenkverfahren und -vorrichtung
US10317852B1 (en) * 2015-10-29 2019-06-11 National Technology & Engineering Solutions Of Sandia, Llc Predictive guidance flight
JP6737222B2 (ja) * 2017-04-14 2020-08-05 株式会社デンソー ステアリング制御装置
US10663260B2 (en) * 2017-11-20 2020-05-26 Bae Systems Information And Electronic Systems Integration Inc. Low cost seeker with mid-course moving target correction
CN112256055B (zh) 2020-10-12 2021-11-05 清华大学 一种采用不动点优化的三体对抗防御预测制导方法

Also Published As

Publication number Publication date
IL301348A (en) 2023-05-01
AU2021366148B2 (en) 2024-07-18
DE102020006465A1 (de) 2022-04-21
IL301348B2 (en) 2024-05-01
AU2021366148A9 (en) 2024-05-02
AU2021366148A1 (en) 2023-06-22
US12228383B2 (en) 2025-02-18
EP4232771A1 (de) 2023-08-30
EP4232771B1 (de) 2024-09-11
KR20230100722A (ko) 2023-07-05
DE102020006465B4 (de) 2022-06-30
IL301348B1 (en) 2024-01-01
WO2022084068A1 (de) 2022-04-28
US20230251070A1 (en) 2023-08-10

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