PL423643A1 - Urządzenie do korygowania trajektorii pocisku rakietowego i sposób korygowania trajektorii - Google Patents

Urządzenie do korygowania trajektorii pocisku rakietowego i sposób korygowania trajektorii

Info

Publication number
PL423643A1
PL423643A1 PL423643A PL42364316A PL423643A1 PL 423643 A1 PL423643 A1 PL 423643A1 PL 423643 A PL423643 A PL 423643A PL 42364316 A PL42364316 A PL 42364316A PL 423643 A1 PL423643 A1 PL 423643A1
Authority
PL
Poland
Prior art keywords
trajectory
correction
projectile
intended
actual
Prior art date
Application number
PL423643A
Other languages
English (en)
Other versions
PL231346B1 (pl
Inventor
André Pfiffer
Original Assignee
Roxel France
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 Roxel France filed Critical Roxel France
Publication of PL423643A1 publication Critical patent/PL423643A1/pl
Publication of PL231346B1 publication Critical patent/PL231346B1/pl

Links

Classifications

    • 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/50—Brake flaps, e.g. inflatable
    • 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
    • F41G7/30—Command link guidance 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
    • 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
    • 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
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

Rozwiązanie dotyczy urządzenia do korygowania (11) trajektorii rzeczywistej pocisku (12), przeznaczonego do przelotu wzdłuż trajektorii nominalnej. Urządzenie (11) zawiera: • impulsator umieszczony na pocisku (12) i przeznaczony do wniesienia korekty bocznej do trajektorii rzeczywistej pocisku (12), • hamulec aerodynamiczny (14) umieszczony na pocisku (12) i przeznaczony do wniesienia korekty osiowej do trajektorii rzeczywistej pocisku (12), • środki do korygowania trajektorii wbudowane w pocisk (12), zdolne do aktywowania impulsatora i hamulca aerodynamicznego (14), • środki do pomiaru (16) trajektorii rzeczywistej pocisku (12), przeznaczone do określenia odchylenia kierunkowego pomiędzy trajektorią rzeczywistą a trajektorią nominalną, • środki obliczeniowe (17) przeznaczone do określenia sekwencji co najmniej jednej korekty w zależności od odchylenia kierunkowego, • środki do transmisji (18) sekwencji ze środków obliczeniowych (17) do środków do korygowania trajektorii.
PL423643A 2015-04-20 2016-04-05 Urządzenie do korygowania trajektorii pocisku rakietowego i sposób korygowania trajektorii PL231346B1 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1553490 2015-04-20
FR1553490A FR3035205B1 (fr) 2015-04-20 2015-04-20 Dispositif de correction de trajectoire d'un projectile et procede de correction de trajectoire
PCT/EP2016/057400 WO2016169760A1 (fr) 2015-04-20 2016-04-05 Dispositif de correction de trajectoire d'un projectile et procede de correction de trajectoire

Publications (2)

Publication Number Publication Date
PL423643A1 true PL423643A1 (pl) 2018-03-26
PL231346B1 PL231346B1 (pl) 2019-02-28

Family

ID=54291367

Family Applications (1)

Application Number Title Priority Date Filing Date
PL423643A PL231346B1 (pl) 2015-04-20 2016-04-05 Urządzenie do korygowania trajektorii pocisku rakietowego i sposób korygowania trajektorii

Country Status (4)

Country Link
FR (1) FR3035205B1 (pl)
PL (1) PL231346B1 (pl)
RO (1) RO132502B1 (pl)
WO (1) WO2016169760A1 (pl)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2543606C2 (de) * 1975-09-30 1986-11-06 Deutsch-Französisches Forschungsinstitut Saint-Louis, Saint-Louis Anordnung zur Flugbahnkorrektur eines rotierenden Geschosses
FR2627269B1 (fr) * 1988-02-17 1993-05-14 Thomson Csf Systeme de correction de la trajectoire d'un projectile
FR2761767B1 (fr) * 1997-04-03 1999-05-14 Giat Ind Sa Procede de programmation en vol d'un instant de declenchement d'un element de projectile, conduite de tir et fusee mettant en oeuvre un tel procede
EP1366339B1 (en) * 2001-02-01 2009-07-29 BAE Systems Land & Armaments L.P. 2-d projectile trajectory corrector
DE102005052474B3 (de) * 2005-11-03 2007-07-12 Junghans Feinwerktechnik Gmbh & Co. Kg Drallstbilisiertes Artillerieprojektil

Also Published As

Publication number Publication date
RO132502A2 (ro) 2018-04-27
RO132502B1 (ro) 2023-10-30
FR3035205A1 (fr) 2016-10-21
PL231346B1 (pl) 2019-02-28
FR3035205B1 (fr) 2018-10-05
WO2016169760A1 (fr) 2016-10-27

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