Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F41—WEAPONS
  • F41G—WEAPON SIGHTS; AIMING
  • F41G7/00—Direction control systems for self-propelled missiles
  • F41G7/006—Guided missiles training or simulation devices
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F41—WEAPONS
  • F41G—WEAPON SIGHTS; AIMING
  • F41G3/00—Aiming or laying means
  • F41G3/26—Teaching or practice apparatus for gun-aiming or gun-laying
  • F41G3/2616—Teaching or practice apparatus for gun-aiming or gun-laying using a light emitting device
  • F41G3/2694—Teaching or practice apparatus for gun-aiming or gun-laying using a light emitting device for simulating a target

Definitions

• the projectile is a fictitious projectile; a computer provides the definition of the position of the fictitious projectile, compares this position with that of the intended target, then assesses the quality of the shot by determining, in particular, whether the aiming (or aimed) would, if the shot were real, lead the projectile has an impact on the target.
• the simulator Before launching the shooting exercise, the simulator must be harmonized so as to ensure the correspondence of the projected image, or returned in the micromonitor, with the acquisition space of the camera which locates the laser beam linked to the student. In addition, the student may experience feelings of discomfort due to the difference between what he feels at the time of shooting and what he sees on the screen.
• Such devices therefore have the disadvantage of not offering realism and sufficient comfort of use for shooters.
• These devices also have the disadvantage of requiring the use of a laser system, as well as an acquisition camera, which leads to difficulties in harmonization and implementation.
• the object of the invention is precisely to remedy the drawbacks of the devices described above. To this end, it offers a device for simulating missile launching on the shoulder or on a tripod aimed at improving the realism and the comfort of use of shooters during their training by immersing them in a virtual space.
• the invention relates to a missile firing simulator for training missile shooters on the shoulder or on a tripod, on fixed or mobile targets, which comprises: - at least one firing station equipped with means for fictitious firing;
• the instructor station includes a video screen associated with decision means from which an instructor chooses a virtual scenario relating to the firing range, the type of missile and the firing conditions;
• the shooting station includes means of spatial location;
• the image display means comprise a display device displaying virtual images, in real size, representative of the shooter's field of vision in the scenario chosen by the instructor and a micromonitor placed in the shooting station and displaying the same images than those of the display device, but magnified according to a predefined coefficient;
• the image processing means comprise a central processing unit associated with an image generator generating the images of the instructor station, the images of the micromonitor and the images of the display device.
• the image generator is capable of generating two images simultaneously on the instructor station, one of the images being a top view of the shooting range and the other image representing the field of vision of the instructor in the process of 'observe the shooting scene.
• the simulator is capable of generating a different reticle for each type of weapon system. It can also generate images of the shooting range according to a variable brightness, representative of climatic and sunshine variations.
• the simulator comprises means for restoring the disturbances caused by the departure of the missile.
• the instructor station includes means for memorizing each shooting exercise to allow a subsequent analysis of the result of the shooting.
• FIG. 1 shows schematically the different elements constituting the device of the invention, as well as their connections;
• the invention relates to a missile launching simulator intended for training missile shooters on mobile targets, by integrating the shooter into a virtual space.
• the simulator which will be described is intended to facilitate training in firing missiles at a moving target which may be a land vehicle, for example a tank, or else a flying object, for example a helicopter. We will therefore speak, in the following description, simply of mobile target.
• This missile launching simulator revolves around a central unit responsible for data processing and two workstations: an instructor station and a gunner station.
• the term “shooter station” is used to mean the assembly consisting of a suitable firing station, an ammunition tube equipped with a possible load-shedding system and means for visualizing the shooting range.
• the adapted shooting station is an identical shooting station to a real shooting station, from an ergonomic point of view (position of controls, masses, centering) but whose functions have been replaced by functions linked to simulation.
• Such a firing station is described, in particular, in patent application FR-A-2 685 464, filed in the name of the applicant.
• the adapted shooting station of the invention does not have a sighting system; this is replaced by a micromonitor on which the virtual images appearing representing the field of vision of the shooter, according to a format (dimensions, magnification) identical to that of the view through the sighting system of a shooting station real. On this micromonitor, virtual images are displayed representing the virtual space in which the shooter evolves, "in exercise”.
• the instructor can also choose other shooting conditions, such as the climatic and sun conditions in which the shooter will have to work: day, night, fog, etc. These shooting conditions can be modified by the instructor, even during exercise.
• the instructor station may include a memorization means intended to memorize the scenarios, as well as the result of the shots, so as to allow, later, the analysis of the missile launch.
• the shooter station includes a disturbance restitution device, referenced 6.
• the position sensor can also be a gyrometric sensor, which has the advantage of being precise and insensitive to the surrounding electromagnetic waves.
• Other types of 3D position sensors can also be envisaged.
• the central unit 8 has the role of interpreting the commands of the instructor, of restoring the scenario chosen by the instructor at the instructor station and at the shooter station, of taking into account the command of fire and of allowing, if necessary, the implementation of disturbance restitution devices.
• This central unit can be, for example, a generator of synthetic images, or even a PC type computer.
• the instructions relating to this scenario are sent to the central unit 8 which, in association with an image generator 10, generates all the images necessary for the exercise. More specifically, it is the image generator 10 which forms all the images from the data supplied by the central unit 8. It generates, in particular, the image or images for the instructor station. According to the preferred embodiment of the invention, the instructor station displays two images: a map of the shooting range and a view representing the instructor's field of vision. when the latter looks at the shooter. The image generator 10 also generates two other images intended for the shooter station.
• FIG. 2 shows this device for restoring the disturbances caused by the launching of the missile.
• This device comprises a system of masses ml, m2, positioned in the launch tube, and ejected from the tube during the fictitious launch of the missile.
• This device further comprises proximity sensors cl, c2 arranged on the axis where the electromagnetic masses are fixed. These sensors are used to detect the presence of the masses in order to know whether or not it is necessary to supply them with energy, that is to say in order to know whether these masses should be released or not.
• these proximity sensors supply, to a mass control unit 11, information relating to the presence or not of the masses.
• This control unit 11 also receives information relating to the firing control as well as the energy supply necessary to drop the masses ml and m2.
• This disturbance restitution device further comprises a wire traction system, referenced 12, the role of which is to restore the disturbances due to the wire traction force on the firing station, when the missile is guided.
• This wire traction unit 12 is controlled by a COM2 command which is generated by the simulator after a time ⁇ t after the departure of the missile. So that the traction of the wire is always exerted in the direction of the missile, as is the case for the firing stations real, the wire traction system 12 is controlled by the position relative to the firing station with respect to the missile, by a servo motor 13, controlled by a command C0M1.

Landscapes

• Engineering & Computer Science (AREA)
• General Engineering & Computer Science (AREA)
• Radar, Positioning & Navigation (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
• Processing Or Creating Images (AREA)
• Train Traffic Observation, Control, And Security (AREA)
• Optical Radar Systems And Details Thereof (AREA)

Applications Claiming Priority (3)

Publications (2)

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ID=9515140

Family Applications (1)

Country Status (12)

Families Citing this family (35)

Family Cites Families (27)

• 1997
  • 1997-12-24 FR FR9716517A patent/FR2772908B1/fr not_active Expired - Lifetime
• 1998
  • 1998-12-23 WO PCT/FR1998/002846 patent/WO1999034163A1/fr active IP Right Grant
  • 1998-12-23 BR BR9807380-0A patent/BR9807380A/pt not_active IP Right Cessation
  • 1998-12-23 DE DE69812912T patent/DE69812912T2/de not_active Expired - Lifetime
  • 1998-12-23 JP JP53459099A patent/JP4027436B2/ja not_active Expired - Fee Related
  • 1998-12-23 CA CA002282088A patent/CA2282088C/fr not_active Expired - Lifetime
  • 1998-12-23 IL IL13142698A patent/IL131426A/en not_active IP Right Cessation
  • 1998-12-23 EP EP98963606A patent/EP0961913B1/de not_active Revoked
  • 1998-12-23 US US09/367,112 patent/US6296486B1/en not_active Expired - Fee Related
  • 1998-12-23 TR TR1999/02008T patent/TR199902008T1/xx unknown
  • 1998-12-23 ES ES98963606T patent/ES2195436T3/es not_active Expired - Lifetime
• 1999
  • 1999-08-24 NO NO19994090A patent/NO317683B1/no not_active IP Right Cessation

Non-Patent Citations (1)

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