ATE289052T1 - Verfahren zur steuerung eines flugkörpers - Google Patents

Verfahren zur steuerung eines flugkörpers

Info

Publication number
ATE289052T1
ATE289052T1 AT01270743T AT01270743T ATE289052T1 AT E289052 T1 ATE289052 T1 AT E289052T1 AT 01270743 T AT01270743 T AT 01270743T AT 01270743 T AT01270743 T AT 01270743T AT E289052 T1 ATE289052 T1 AT E289052T1
Authority
AT
Austria
Prior art keywords
missile
guidance
final phase
target
principle
Prior art date
Application number
AT01270743T
Other languages
English (en)
Inventor
Magnus Andersson
Stefan Ljung
Joakim Wallbing
Original Assignee
Saab 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 Ab filed Critical Saab Ab
Application granted granted Critical
Publication of ATE289052T1 publication Critical patent/ATE289052T1/de

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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Catching Or Destruction (AREA)
  • Seats For Vehicles (AREA)
  • Control Of Vending Devices And Auxiliary Devices For Vending Devices (AREA)
AT01270743T 2000-12-13 2001-12-11 Verfahren zur steuerung eines flugkörpers ATE289052T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0004596A SE522565C2 (sv) 2000-12-13 2000-12-13 Förfarande för styrning av en missil
PCT/SE2001/002733 WO2002048636A1 (en) 2000-12-13 2001-12-11 Method for controlling a missile

Publications (1)

Publication Number Publication Date
ATE289052T1 true ATE289052T1 (de) 2005-02-15

Family

ID=20282202

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01270743T ATE289052T1 (de) 2000-12-13 2001-12-11 Verfahren zur steuerung eines flugkörpers

Country Status (7)

Country Link
EP (1) EP1352206B1 (de)
AT (1) ATE289052T1 (de)
AU (1) AU2002221244A1 (de)
DE (1) DE60108902T2 (de)
ES (1) ES2233561T3 (de)
SE (1) SE522565C2 (de)
WO (1) WO2002048636A1 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7446291B1 (en) * 2005-10-03 2008-11-04 Lockheed Martin Corporation Augmented proportional navigation guidance law using angular acceleration measurements
RU2542691C1 (ru) * 2013-11-22 2015-02-20 Открытое акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Способ вывода ракеты в зону захвата цели головкой самонаведения и система для его осуществления (варианты)
CN104298246B (zh) * 2014-09-05 2017-02-08 湖北航天技术研究院总体设计所 一种盘旋飞行轨迹的导引律设计方法及系统
CN108398959A (zh) * 2018-03-28 2018-08-14 北京临近空间飞行器系统工程研究所 一种高超声速滑翔飞行器快速下压制导控制方法
CN109558685B (zh) * 2018-12-05 2021-07-13 北京航空航天大学 弹体支点判定方法、装置、存储介质及电子设备
CN111290427B (zh) * 2018-12-06 2021-07-09 北京理工大学 抗高过载的飞行器侧偏修正系统

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3303763A1 (de) * 1983-02-04 1984-08-09 Diehl GmbH & Co, 8500 Nürnberg Verfahren zur zielansteuerung eines projektils und zum bestimmen dessen ballistischer flugbahn sowie vorrichtungen zum ausueben der verfahren
FR2626677B1 (fr) * 1988-02-01 1990-06-22 Thomson Csf Systeme de radionavigation
US5647558A (en) * 1995-02-14 1997-07-15 Bofors Ab Method and apparatus for radial thrust trajectory correction of a ballistic projectile

Also Published As

Publication number Publication date
DE60108902D1 (de) 2005-03-17
DE60108902T2 (de) 2006-03-02
SE0004596L (sv) 2002-06-14
SE522565C2 (sv) 2004-02-17
EP1352206B1 (de) 2005-02-09
SE0004596D0 (sv) 2000-12-13
AU2002221244A1 (en) 2002-06-24
WO2002048636A1 (en) 2002-06-20
ES2233561T3 (es) 2005-06-16
EP1352206A1 (de) 2003-10-15

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Legal Events

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