FR2663731B1 - SERVO SYSTEM FOR SELF-ROTATING PROJECTILE. - Google Patents

SERVO SYSTEM FOR SELF-ROTATING PROJECTILE.

Info

Publication number
FR2663731B1
FR2663731B1 FR9007785A FR9007785A FR2663731B1 FR 2663731 B1 FR2663731 B1 FR 2663731B1 FR 9007785 A FR9007785 A FR 9007785A FR 9007785 A FR9007785 A FR 9007785A FR 2663731 B1 FR2663731 B1 FR 2663731B1
Authority
FR
France
Prior art keywords
self
servo system
rotating projectile
projectile
rotating
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
FR9007785A
Other languages
French (fr)
Other versions
FR2663731A1 (en
Inventor
Stauff Emile
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR9007785A priority Critical patent/FR2663731B1/en
Publication of FR2663731A1 publication Critical patent/FR2663731A1/en
Application granted granted Critical
Publication of FR2663731B1 publication Critical patent/FR2663731B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F42B10/60—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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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
    • G05D1/108—Simultaneous control of position or course in three dimensions specially adapted for missiles animated with a rolling movement
FR9007785A 1990-06-21 1990-06-21 SERVO SYSTEM FOR SELF-ROTATING PROJECTILE. Expired - Lifetime FR2663731B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9007785A FR2663731B1 (en) 1990-06-21 1990-06-21 SERVO SYSTEM FOR SELF-ROTATING PROJECTILE.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9007785A FR2663731B1 (en) 1990-06-21 1990-06-21 SERVO SYSTEM FOR SELF-ROTATING PROJECTILE.

Publications (2)

Publication Number Publication Date
FR2663731A1 FR2663731A1 (en) 1991-12-27
FR2663731B1 true FR2663731B1 (en) 1992-09-11

Family

ID=9397867

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9007785A Expired - Lifetime FR2663731B1 (en) 1990-06-21 1990-06-21 SERVO SYSTEM FOR SELF-ROTATING PROJECTILE.

Country Status (1)

Country Link
FR (1) FR2663731B1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4410326C2 (en) * 1994-03-25 1998-07-02 Rheinmetall Ind Ag Projectile with a device for trajectory correction
US6928400B2 (en) 2001-10-02 2005-08-09 Raytheon Company Method for designing a deployment mechanism
CA2499956C (en) * 2002-11-18 2009-02-03 Raytheon Company Method for designing a fin deployment mechanism
IL227280A (en) * 2013-07-01 2016-03-31 Shmuel Goldberg Reduction of rocket jet stream dispersion

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2504703B1 (en) * 1981-04-24 1986-09-05 Stauff Emile SYSTEM FOR CONTROLLING A PROJECTILE TO AN AXIAL REFERENCE TO ELIMINATE THE WIND EFFECT

Also Published As

Publication number Publication date
FR2663731A1 (en) 1991-12-27

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Legal Events

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ST Notification of lapse
ST Notification of lapse