| SELEX GALILEO S.P.A. Patent applications |
| Patent application number | Title | Published |
|---|
| 20130181047 | OPTOELECTRONIC DIGITAL APPARATUS FOR ASSISTING AN OPERATOR IN DETERMINING THE SHOOTING ATTITUDE TO BE GIVEN TO A HAND-HELD GRENADE LAUNCHER SO AS TO STRIKE A MOVING TARGET, AND RESPECTIVE OPERATION METHOD - An embodiment of an optoelectronic apparatus for assisting an operator in determining the shooting attitude to give to a hand-held grenade launcher so as to strike a moving target including an electronic processing unit configured so as to: measure the pitch angle and the heading angle of the grenade launcher and the distance of the target when the grenade launcher is moved by the operator during the pointing of the moving target, determine position data indicative of the positions of the moving target, determine a future impact time of the grenade on the target on the basis of position data and of data indicative of the ballistics of the grenade, determine a shooting attitude of the target on the basis of the impact time, measure the pitch angle and heading angle indicating the attitude imparted to the grenade launcher by the operator, compute a pitch difference between the shooting pitch angle and the pitch angle measured and a heading difference between the shooting heading angle and the heading angle measured, communicate to the operator the variation of pitch and/or heading to be given to the grenade launcher so that the pitch and/or heading difference is zero. | 07-18-2013 |
| 20130091754 | ELECTRONIC APPARATUS FOR DETERMINING THE ATTITUDE OF A WEAPON AND OPERATING METHOD THEREOF - An embodiment of an apparatus for determining the attitude angles of a weapon includes a number of accelerometers for measuring the components of the acceleration of the weapon along the axes of a first reference system integral with weapon; a number of gyroscopes configured in such a way to measure the components of the angular speed of the weapon along the axes of the reference body; and a processing unit configured to compute a number of actual attitude angles of the weapon under dynamic conditions based on the components of the angular speed; determine a number of static attitude angles of the weapon under static conditions of the weapon based on the components of the acceleration; and correct the components of angular speed according to static attitude angles and to the actual attitude angles. | 04-18-2013 |
| 20110001011 | Assisted In-Flight Refuelling System - An assisted in-flight refuelling system having a tanker aircraft equipped with a drogue; a fuel take-on aircraft equipped with a probe; and a drogue-probe coupling assist system designed to determine a first distance between the drogue and the take-on aircraft/probe, a second distance between the tanker aircraft and the drogue, and a third distance between the tanker aircraft and the take-on aircraft. The drogue-probe coupling assist system is also designed to determine information relative to the necessary movement of the drogue and/or the necessary movement of the take-on aircraft to couple the drogue to the probe, as a function of the first, second, and third distance. | 01-06-2011 |
