초록 ▼

The invention relates to a system for target designation and/or illumination in a scene, that is designed to be attached to an aircraft comprising one optical path fitted with a matrix sensor forming an image of the scene, each image corresponding to an instantaneous field centered around a line of

The invention relates to a system for target designation and/or illumination in a scene, that is designed to be attached to an aircraft comprising one optical path fitted with a matrix sensor forming an image of the scene, each image corresponding to an instantaneous field centered around a line of sight LV, and fitted with a device for deflecting the LV at a determined speed Vd making it possible to carry out a scan in order to perform the target designation and illumination function. The system comprises an additional device for deflecting the LV at a speed Vr making it possible to carry out a counter-scan in order also to perform an air reconnaissance function.

대표청구항 ▼

1. A system for laser target designation and/or illumination in a scene, that is adapted to be attached to an aircraft, and to be oriented in an instantaneous field greater than 60° in which a line of sight LV is centered, said system comprising: at least one telemetry and/or target designation and/

1. A system for laser target designation and/or illumination in a scene, that is adapted to be attached to an aircraft, and to be oriented in an instantaneous field greater than 60° in which a line of sight LV is centered, said system comprising: at least one telemetry and/or target designation and/or illumination laser;at least one optical channel fitted with a matrix sensor forming an image of the scene, each image corresponding to the instantaneous field centered around the line of sight LV, and fitted with a device for deflecting the line of sight LV at a determined speed Vd so as to carry out a scan in order to perform a laser target designation and illumination function; andan additional device for deflecting the line of sight LV at a speed Vr so as to carry out a counter-scan in order to perform an air reconnaissance function,wherein the additional device comprises an optical deflecting element for deflecting the line of sight LV and a device for moving the optical deflecting element at the speed Vr. 2. The system as claimed in claim 1, further comprising a sensor configured to operate for a period D, and configured to incorporate a photonic signal corresponding to the instantaneous field for a duration I, wherein the optical deflecting element is movable by the device for moving the deflecting element at the speed Vr, in order to compensate for the movement of the system adapted to be attached to the aircraft, over a minimal amplitude equal to the instantaneous field×I/D, at a minimal frequency of 5 Hz in a direction that is lateral or parallel to a path of the aircraft. 3. The system as claimed in claim 2, wherein the lateral direction is perpendicular to the path of the aircraft. 4. The system as claimed in claim 1, wherein the system further comprises a bending mirror configured to perform the laser target designation and illumination function, and the mirror is an optical element for deflecting the line of sight LV. 5. The system as claimed in claim 1, wherein the optical deflecting element is an optical strip. 6. The system as claimed in claim 1, wherein the scene is at least one of terrestrial, maritime, aerial or spatial. 7. The system as claimed in claim 1, further comprising an IR optical channel and/or a near-infrared channel and/or a visible channel. 8. An air reconnaissance method of forming images, each image corresponding to an instantaneous field centered around a line of sight LV, said method comprising the steps of: scanning the line of sight LV with a probe element fitted with a matrix sensor, in a determined direction at least during the time of integration of the sensor,counter-scanning in a direction opposite to the determined direction by a deflecting device in order to stabilize the line of sight LV during integration of the sensor,deactivating the counter-scan, andlaser target designation and/or illumination by the matrix sensor during said step of deactivating the counter-scan,wherein an additional device comprises an optical deflecting element for deflecting the line of sight LV and a device for moving the optical deflecting element at a speed Vr.