DE60101449D1 - Regelung der Reichweite eines raketenangetriebenen Projektils - Google Patents

Regelung der Reichweite eines raketenangetriebenen Projektils

Info

Publication number
DE60101449D1
DE60101449D1 DE60101449T DE60101449T DE60101449D1 DE 60101449 D1 DE60101449 D1 DE 60101449D1 DE 60101449 T DE60101449 T DE 60101449T DE 60101449 T DE60101449 T DE 60101449T DE 60101449 D1 DE60101449 D1 DE 60101449D1
Authority
DE
Germany
Prior art keywords
projectile
value
range
actual
point
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
DE60101449T
Other languages
English (en)
Other versions
DE60101449T2 (de
Inventor
Sven Komstadius
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.)
Saab AB
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
Publication of DE60101449D1 publication Critical patent/DE60101449D1/de
Application granted granted Critical
Publication of DE60101449T2 publication Critical patent/DE60101449T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/92—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control incorporating means for reversing or terminating thrust
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins
    • 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
    • F42B10/66—Steering by varying intensity or direction of thrust
    • 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
    • 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
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Toys (AREA)
  • Testing Of Engines (AREA)
DE60101449T 2000-11-03 2001-10-12 Regelung der Reichweite eines raketenangetriebenen Projektils Expired - Lifetime DE60101449T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0004022A SE516094C2 (sv) 2000-11-03 2000-11-03 Metod och anordning vid en reketmotordriven projektil
SE0004022 2000-11-03

Publications (2)

Publication Number Publication Date
DE60101449D1 true DE60101449D1 (de) 2004-01-22
DE60101449T2 DE60101449T2 (de) 2004-06-09

Family

ID=20281686

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60101449T Expired - Lifetime DE60101449T2 (de) 2000-11-03 2001-10-12 Regelung der Reichweite eines raketenangetriebenen Projektils

Country Status (5)

Country Link
EP (1) EP1225327B1 (de)
AT (1) ATE256250T1 (de)
DE (1) DE60101449T2 (de)
ES (1) ES2208509T3 (de)
SE (1) SE516094C2 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE531815C2 (sv) * 2007-10-19 2009-08-11 Bae Systems Bofors Ab Sätt att variera skottvidd och verkan i mål för granat och granat utformad därför

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3176518A (en) * 1961-08-24 1965-04-06 Systron Donner Corp Dual acceleration range integrating accelerometer
US3737122A (en) * 1971-05-07 1973-06-05 Singer General Precision Tactical missile range control system
US3890901A (en) * 1972-05-22 1975-06-24 Us Navy Digital electronic safety and arming system
US4013012A (en) * 1974-11-18 1977-03-22 Altus Corporation Electronic safe arming and fuzing system
US4428293A (en) * 1980-12-19 1984-01-31 United Technologies Corporation Gun-launched variable thrust ramjet projectile
US5779576A (en) * 1996-08-20 1998-07-14 Smith Engineering Throw-measuring football

Also Published As

Publication number Publication date
ES2208509T3 (es) 2004-06-16
SE0004022D0 (sv) 2000-11-03
SE0004022L (sv) 2001-11-19
ATE256250T1 (de) 2003-12-15
SE516094C2 (sv) 2001-11-19
EP1225327A1 (de) 2002-07-24
EP1225327B1 (de) 2003-12-10
DE60101449T2 (de) 2004-06-09

Similar Documents

Publication Publication Date Title
JPS55161923A (en) Fuel control device for gas turbine engine
ZA200604101B (en) Method and device for setting the fuse and/or correcting the ignition time of a projectile
JPS54108133A (en) Electronic engine control system
JPS57102527A (en) Fuel injection nozzle unit
DK0925516T3 (da) Fremgangsmåde til bestemmelse af et anslagspunkt for et affyret projektil i forhold til målet
JPS55139970A (en) Ignition timing controller at the time of starting
DE60101449D1 (de) Regelung der Reichweite eines raketenangetriebenen Projektils
ZA200300259B (en) Method and device for compensating firing errors and system computer for weapon system.
US4450817A (en) Method and apparatus for controlling fuel injection timing for compression ignition engines
JPS5786549A (en) Air fuel ratio controller
JPS55131532A (en) Fuel controller for gas turbine engine
KR950001447A (ko) 캠축의 각도 위치를 조절하는 방법 및 장치
JPS5623565A (en) Method for feedback control of ignition time
KR950019092A (ko) 경사로 주행시 엔진 동작 제어장치 및 그 방법
JPH06257995A (ja) 射出装置
RU2000103634A (ru) Способ командного телеуправления ракетой
SE522568C2 (sv) Förfarande för hastighetskompensering av en RSV-stråle, samt robot
JPS56146027A (en) Controlled device for maximum injection quantity of fuel injection pump
JPS557335A (en) Soft start controller for working machine
RU2004109801A (ru) Способ управления ракетой
JPS56121834A (en) Air-fuel ratio controller with correction for starting operation
JPS56146026A (en) Controlling method for maximum injection quantity of fuel injection pump
EP0333701A3 (en) Method for controlling and regulating an automotive engine
JPH1162685A (ja) ディーゼルエンジンの電子制御式調速装置
JPS5712218A (en) Gas combustion controller

Legal Events

Date Code Title Description
8364 No opposition during term of opposition