GB1294291A - Method and system for establishing a correct lead when firing at a moving target - Google Patents

Method and system for establishing a correct lead when firing at a moving target

Info

Publication number
GB1294291A
GB1294291A GB270/70A GB27070A GB1294291A GB 1294291 A GB1294291 A GB 1294291A GB 270/70 A GB270/70 A GB 270/70A GB 27070 A GB27070 A GB 27070A GB 1294291 A GB1294291 A GB 1294291A
Authority
GB
United Kingdom
Prior art keywords
sight
line
target
proportional
signals
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
Application number
GB270/70A
Inventor
Rune Torsten Isidor Erhard
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 Bofors AB
Original Assignee
Bofors 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 Bofors AB filed Critical Bofors AB
Publication of GB1294291A publication Critical patent/GB1294291A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G3/00Aiming or laying means
    • F41G3/06Aiming or laying means with rangefinder

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1294291 Sights and methods of sighting BOFORS AB 2 Jan 1970 [3 Jan 1969] 270/70 Heading F3C [Also in Division G4] In a method for providing a correct lead when firing a projectile at a moving target, the sight is maintained pointed directly at the target, and the angular velocity of the line of sight is integrated over a predetermined limited interval during which the direction of fire of the weapon is moved uniformly with the line of sight, whereafter the line of sight and the direction of fire are deflected from each other by an angle proportional to the result of integration and in such sense that the direction of fire will lead the line of sight. As shown, a manually operated lever 5 controlling signal sources 51 and 52 determines the angular velocity of the gun barrel in azimuth and in elevation, respectively, by means of the servo motors M1, M2 comparators C1, C2, amplifiers F1, F2, and tachogenerators T1, T2, the signals from which are fed back in opposition to the'comparators. A sighting instrument mounted on the gun barrel is similarly movable in azimuth and elevation with respect to the barrel by servo motors M3 and M4 which have predetermined starting positions in which the line of sight is parallel to to the barrel. Potentiometers P1 and P2 feed back signals to comparators C3 and C4 which are proportional to the angle of rotation of the motors, whereby the motors rotate the sighting instrument through angles proportional to control signals from amplifiers F3 and F4, respectively and inversely proportional to the signal-which is proportional to the mean velocity of the projectile-from amplifier F5. When the line of sight shown by the dotted line in Fig. 3, has been accurately aimed at the moving target, shown by the full line, a timer T having a time span # proportional to the range to the target, is energized, at time # 1 Fig. 3, to close switches K1 and apply the tachogenerator signals from T1 and T2 to integrators I1 and I2, for computing the lead angles in azimuth and elevation required due to movement of the target, a correcting factor involving the superelevation being provided at the output of amplifier F6, and another involving projectile rotation and wind forces being provided at the output of amplifier F7 at the termination # 2 of the timer interval, switches K1 are opened and switches K2, K4, and K5 closed to apply the integrated signals and correcting factors to amplifiers F3 and F4, which then rotate motors M3 and M4 to deflect the line of sight, to lag the target, through the required lead angle # t . Thereafter, lever 5 is again operated to aim the sight at the target, and thereby deflect the gun barrel, shown by the dash-dot curve, through the required lead angle, whereafter firing can commence. In a modified arrangement, which, avoids the manual reaiming of the sight, tachogenerators T3 and T4, generating signals proportional to the rates of rotation of servomotors M3 and M4, are coupled comparators C1 and C2, to apply the signals to motors M1 and M2 in a sense assisting the control signals from the signal generators S1 and S2, whereby when the motors M3 and M4 start to rotate the gun barrel is given increased azimuthal and elevational angular velocities, such that the sight remains aimed at the target and the barrel is deflected through the required lead angle. If the sighting instrument is not mounted on a layable portion of the gun, the servomotors for the latter are supplied with control signals derived from position detectors coupled to the servomotors of the sighting instrument.
GB270/70A 1969-01-03 1970-01-02 Method and system for establishing a correct lead when firing at a moving target Expired GB1294291A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE00096/69A SE331245B (en) 1969-01-03 1969-01-03

Publications (1)

Publication Number Publication Date
GB1294291A true GB1294291A (en) 1972-10-25

Family

ID=20256033

Family Applications (1)

Application Number Title Priority Date Filing Date
GB270/70A Expired GB1294291A (en) 1969-01-03 1970-01-02 Method and system for establishing a correct lead when firing at a moving target

Country Status (11)

Country Link
US (1) US3685159A (en)
JP (1) JPS493677B1 (en)
BE (1) BE743927A (en)
CA (1) CA930216A (en)
CH (1) CH535934A (en)
DE (1) DE1965559A1 (en)
FR (1) FR2027717A1 (en)
GB (1) GB1294291A (en)
NL (1) NL6919680A (en)
NO (1) NO124962B (en)
SE (1) SE331245B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2447391C2 (en) * 2010-04-29 2012-04-10 Общество с ограниченной ответственностью "АВТЭКС" Safe method of firing (versions) and safe sight for firing at moving targets
WO2013126110A2 (en) 2011-11-30 2013-08-29 General Dynamics Armament And Technical Products, Inc. Gun sight for use with superelevating weapon
GB2625381A (en) * 2022-12-16 2024-06-19 Raytheon Systems Ltd A guidance method and system

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE355664B (en) * 1971-02-26 1973-04-30 Bofors Ab
US3845276A (en) * 1971-12-17 1974-10-29 Hughes Aircraft Co Laser-sight and computer for anti-aircraft gun fire control system
US4020407A (en) * 1973-03-02 1977-04-26 Etat Francais Control system for tracking a moving target
SE390221B (en) * 1974-10-21 1976-12-06 Bofors Ab LOGIC CONTROLLED INTEGRATOR
US4004729A (en) * 1975-11-07 1977-01-25 Lockheed Electronics Co., Inc. Automated fire control apparatus
SE420765B (en) * 1978-01-18 1981-10-26 Bofors Ab DEVICE FOR A WEAPON ORIENTATION
DE3213235A1 (en) * 1982-04-08 1983-10-13 Diehl GmbH & Co, 8500 Nürnberg VISOR DEVICE
SE452057B (en) * 1985-04-16 1987-11-09 John Lorenz Weibull WEAPON RIGHTS, DEDICATED FOR SHOOTING AGAINST TERRIFICIAL TARGETS
US4777861A (en) * 1987-01-16 1988-10-18 Recon/Optical, Inc. Missile aiming sight
SE468330B (en) * 1991-04-17 1992-12-14 Saab Instr Ab DEVICE FOR AIM OF A MOBILE OBJECTIVE AND ORIENTATION OF AN AIRFIRE SPEED OR SIMILAR TO THE SAME
DE59903384D1 (en) * 1998-10-08 2002-12-19 Contraves Pyrotec Ag Method for correcting a preprogrammed triggering of a process in a spin-stabilized projectile, device for carrying out the method and use of the device
SE519151E5 (en) * 2001-11-19 2013-07-30 Bae Systems Bofors Ab Weapon sight with sight sensors intended for vehicles, vessels or equivalent
DE50204077D1 (en) * 2002-01-16 2005-10-06 Contraves Ag Method and apparatus for compensating shooting defects and system computers for weapon systems
US6769347B1 (en) 2002-11-26 2004-08-03 Recon/Optical, Inc. Dual elevation weapon station and method of use
US8646374B2 (en) * 2010-07-27 2014-02-11 Raytheon Company Weapon station and associated method
WO2014186049A2 (en) * 2013-03-21 2014-11-20 Kms Consulting, Llc Apparatus for correcting ballistic errors using laser induced fluorescent (strobe) tracers
FR3019279B1 (en) 2014-03-28 2018-06-22 Safran Electronics & Defense OPTRONIC ARMY TURTLE
US9638502B1 (en) * 2014-08-18 2017-05-02 Rockwell Collins, Inc. Pulse error correction for spinning vehicles
US10488155B2 (en) * 2015-01-23 2019-11-26 Raytheon Company Method and apparatus for electro-mechanical super-elevation
EP3420300A4 (en) * 2016-02-24 2019-09-04 Pautler, James Anthony Dynamic sight
DE102016113262B4 (en) * 2016-07-19 2023-06-15 Michael Hahn Hunting firearm and method of improving marksmanship
CN115480275B (en) * 2022-09-15 2023-08-08 中华人民共和国广东海事局 Motion state acquisition method and device, computer equipment and storage medium

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2447391C2 (en) * 2010-04-29 2012-04-10 Общество с ограниченной ответственностью "АВТЭКС" Safe method of firing (versions) and safe sight for firing at moving targets
WO2013126110A2 (en) 2011-11-30 2013-08-29 General Dynamics Armament And Technical Products, Inc. Gun sight for use with superelevating weapon
EP2800942A4 (en) * 2011-11-30 2015-07-15 Gen Dynamics Ots Inc Gun sight for use with superelevating weapon
AU2012370428B2 (en) * 2011-11-30 2016-06-16 General Dynamics-Ots, Inc. Gun sight for use with superelevating weapon
GB2625381A (en) * 2022-12-16 2024-06-19 Raytheon Systems Ltd A guidance method and system

Also Published As

Publication number Publication date
CH535934A (en) 1973-04-15
SE331245B (en) 1970-12-14
JPS493677B1 (en) 1974-01-28
NO124962B (en) 1972-06-26
DE1965559A1 (en) 1971-03-11
FR2027717A1 (en) 1970-10-02
NL6919680A (en) 1970-07-07
US3685159A (en) 1972-08-22
CA930216A (en) 1973-07-17
BE743927A (en) 1970-05-28

Similar Documents

Publication Publication Date Title
GB1294291A (en) Method and system for establishing a correct lead when firing at a moving target
GB1381945A (en) Gun
GB1108072A (en) Anti-aircraft weapon carriage
US3169727A (en) Multiple flight course second order missile programmer
GB1380531A (en) Fire ranging method for launchers of self-propelled missiles
US3798420A (en) Method of controlling motor-driven devices adapted to be directed onto moving targets and apparatus for applying the method
GB1062473A (en) Process for controlling the motion of a first body as a function of the position of a second body, and device for implementing this process
GB1277251A (en) Ballistic computer
GB1309793A (en) Firing-control system
GB1441127A (en) Guidance system for an anti-aircraft missile
US3741502A (en) Long range missile programmer
US3164339A (en) Missile programmer coast mode provision
US3443476A (en) Control system for rotatable gun platform and optical sight
US3206143A (en) Controller for guiding a missile carrier on the location curve of ballistic firing positions
GB1056815A (en) Fire control system for weapons
GB1377358A (en) Method of advancing the point of impact for passive-location missiles guided by means of proportional navigation in the self-guide phase
GB1064774A (en) Weapon firing control system
US5102064A (en) Missile guidance systems
GB678810A (en) Improvements in or relating to high-frequency direction finding apparatus
GB1446362A (en) Navigation system for guiding a body to impact a moving target
US3712562A (en) Sector gating circuit
GB724896A (en) Improvements in gyro-stabilised control systems for guns and the like
GB1259881A (en) Fire control systems for guns
GB943310A (en) Improvements in or relating to automatic control systems for guiding air-borne missiles
RU1621676C (en) Method of gun orientation and laying at fire from defilade and device for its accomplishment

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee