smart bullet-laser guided


The invention relates to a method and a device for the automated control of driven and unpowered flying objects in a beam tunnel preferably drawn by an X / Y galvanometer system, preferably laser-operated, without absolutely necessary return channel of the object. A non-contact guidance with "soft" planks, which allows the object to change direction, preferably by changing object geometry when exposed to light. A method to accurately control a flying object with minimal effort - preferably without on-board electronics (or minimal number of components of smallest possible volume) - and to let it land pinpoint.


smart bullet-laser guided -2


The invention relates to a method and a device for automated controlling of a projectile (21) which is at least on the lower side partially wrapped in a polymer film. The projectile will be directed in a beam tunnel, which is preferably drawn from an X/Y galvanometer system(8) with sector-dependent different and rolling upcoded signal strength. The Beam tunnel varies signal strengths gradually increasing between tunnel center and outer diameter. At the projectile bottom a signal-reflecting triplesmirror (25) is mounted so that a control unit (4) can perform the projectile position detection. The system is preferably laser operated (6), without any incorporation of mechanical or electronic parts into the projectile (18). It offers non-contact guidance with "soft" planks that allow the projectile to change direction through sidewall (21/19) differences (26) to achieve unprecedented accuracy up to one kilometer range.


smart bullet-laser guided -3


The invention relates to a method for the automated control of a projectile, preferably by means of a galvanometer system in combination with a standing Tem00 beam, when the projectile is to fly beyond the usable range of the galvo system. To be used as projectiles we suggest conventional ammunition and missile projectiles which are provided with polymer walls and triple mirrors.


smart bullet 4&5


The invention represents a method and a device for the automated control of a projectile, preferably by means of a galvanometer system. As projectiles cylindrical rocket projectiles are proposed, which will have fins - that swing out after exiting the barrel – and control flaps – which are polymer-coated on the inner side. The projectile outer wall at the drive propulsion segment is mirrored. A swivel nozzle that is connected to each of the four control flaps via ceramic threads will ensure maneuverability using vector thrust. Also advantageous is the thrust flow deflection by Coanda - or more simple - by vortex effects due to the air flow flowing between the fin and each control flap which will change their individual alignment under the influence of laser light. The device consists of a 4mm diameter and 40mm long solid fuel containing cylinder with an electronic ignition mechanism incorporated in the conical head part and a steering section mounted on the rearmost part of the projectile.