摘要:
A piece of airborne optoelectronic equipment (EO, EO1, EO2) comprising: - at least one image sensor (CI1, CI2), designed to acquire a plurality of images (IMR1, IMR2) of a region (RS) flown over by a carrier (PO1, PO2) of said equipment; and - a data processor (PD) configured or programmed to receive at least one so-called acquired image and transmit same to a display device (EA); characterised in that said data processor is also configured or programmed to: - access a database (BD) of images of said overflown region; - extract, from said database, information making it possible to synthesise a virtual image (IMV) of said region that is viewed by an observer located at a predefined observation point and watching, with a predefined field of view, along a predefined line of sight; - synthesise said virtual image and; - transmit same to said or to another display device. The invention also relates to a method for using such a piece of equipment.
摘要:
The invention relates to a method of telemetry for a target effected by an operator by means of binoculars, which comprises an image sensor (1), a display screen (2), a processing unit and a laser telemeter (4) having a firing window centred on the line of sight of the laser. This method comprises the following steps of: capture by the image sensor (1) of what is called a real image (10), including the image of the target to be telemetered and display on the screen (2) of a corresponding stabilized image (20); calculation by the processing unit of the shift ΔS between the real image (10) and the stabilized image (20); positioning of the stabilized image (20) on a predetermined position P of the display screen; order of firing by the operator; calculation of the shift d = ΔS + Δh, Δh being a predetermined harmonization shift; display on the display screen of an element (23) representative of the telemeter firing window; displacement of this element (23) representative of the firing window towards the position P of the screen, at a rate of displacement smaller than a predetermined speed, and, during this displacement, calculation of the shift d = ΔS + Δh, Δh being a predetermined harmonization shift; and triggering of the laser shot by the processing unit as soon as d