DE69223667T2 - Verfahren zur Kombination der Leitflossensteuerung - Google Patents

Verfahren zur Kombination der Leitflossensteuerung

Info

Publication number
DE69223667T2
DE69223667T2 DE69223667T DE69223667T DE69223667T2 DE 69223667 T2 DE69223667 T2 DE 69223667T2 DE 69223667 T DE69223667 T DE 69223667T DE 69223667 T DE69223667 T DE 69223667T DE 69223667 T2 DE69223667 T2 DE 69223667T2
Authority
DE
Germany
Prior art keywords
control
combining
procedure
fin
control fin
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 - Lifetime
Application number
DE69223667T
Other languages
English (en)
Other versions
DE69223667D1 (de
Inventor
Dennes P Forsmo
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.)
Raytheon Co
Original Assignee
Raytheon Co
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 Raytheon Co filed Critical Raytheon Co
Application granted granted Critical
Publication of DE69223667D1 publication Critical patent/DE69223667D1/de
Publication of DE69223667T2 publication Critical patent/DE69223667T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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

Landscapes

  • 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)
DE69223667T 1991-03-20 1992-03-10 Verfahren zur Kombination der Leitflossensteuerung Expired - Lifetime DE69223667T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/672,279 US5088658A (en) 1991-03-20 1991-03-20 Fin command mixing method

Publications (2)

Publication Number Publication Date
DE69223667D1 DE69223667D1 (de) 1998-02-05
DE69223667T2 true DE69223667T2 (de) 1998-08-27

Family

ID=24697897

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69223667T Expired - Lifetime DE69223667T2 (de) 1991-03-20 1992-03-10 Verfahren zur Kombination der Leitflossensteuerung

Country Status (6)

Country Link
US (1) US5088658A (de)
EP (1) EP0505071B1 (de)
JP (1) JPH05108157A (de)
DE (1) DE69223667T2 (de)
ES (1) ES2110469T3 (de)
GR (1) GR3025938T3 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5593109A (en) * 1995-01-10 1997-01-14 Lucas Western, Inc. Actuator system and method
US5631830A (en) * 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
US5590850A (en) * 1995-06-05 1997-01-07 Hughes Missile Systems Company Blended missile autopilot
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
US6637699B2 (en) 2002-03-25 2003-10-28 Lockheed Martin Corporation Method and apparatus for controlling a trajectory of a projectile
US6921052B2 (en) * 2003-11-28 2005-07-26 The United States Of America As Represented By The Secretary Of The Army Dragless flight control system for flying objects
IL177527A (en) * 2006-08-16 2014-04-30 Rafael Advanced Defense Sys Missile survey targets
FR2909462B1 (fr) * 2006-12-05 2008-12-26 Airbus France Sas Procede et dispositif de controle actif du tangage d'un avion.
US7781709B1 (en) * 2008-05-05 2010-08-24 Sandia Corporation Small caliber guided projectile
WO2011127338A2 (en) * 2010-04-08 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Predictive roll capture
US9037315B2 (en) * 2013-06-06 2015-05-19 Raytheon Company Air vehicle control system and method
US9222755B2 (en) * 2014-02-03 2015-12-29 The Aerospace Corporation Intercepting vehicle and method
CN106081140B (zh) * 2016-07-13 2019-01-22 西藏长源动力科技有限公司 一种炮射无人机自动驾驶仪安装架
CN106444807B (zh) * 2016-09-29 2019-04-12 湖北航天技术研究院总体设计所 一种栅格舵与侧喷流的复合姿态控制方法
RU2632550C1 (ru) * 2016-10-28 2017-10-05 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" Летательный аппарат
US11619473B2 (en) 2021-01-11 2023-04-04 Bae Systems Information And Electronic Systems Integration Inc. Command mixing for roll stabilized guidance kit on gyroscopically stabilized projectile

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2824710A (en) * 1949-01-05 1958-02-25 Albert C Hall Control system for guided missiles
US2967031A (en) * 1956-10-29 1961-01-03 Honeywell Regulator Co Control apparatus for dirigible craft
US3575362A (en) * 1968-10-03 1971-04-20 William M Hammond Adaptive missile control system incorporating a supervisory loop
DE2239398C3 (de) * 1972-08-10 1981-10-15 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Steuervorrichtung für Flugkörper
US3946968A (en) * 1974-08-02 1976-03-30 Raytheon Company Apparatus and method for aerodynamic cross-coupling reduction
US4530476A (en) * 1981-08-12 1985-07-23 E-Systems, Inc. Ordnance delivery system and method including remotely piloted or programmable aircraft with yaw-to-turn guidance system

Also Published As

Publication number Publication date
JPH05108157A (ja) 1993-04-30
GR3025938T3 (en) 1998-04-30
EP0505071B1 (de) 1997-12-29
EP0505071A2 (de) 1992-09-23
DE69223667D1 (de) 1998-02-05
EP0505071A3 (en) 1993-10-20
ES2110469T3 (es) 1998-02-16
US5088658A (en) 1992-02-18

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition