Abstract:
A computer-implemented method for detecting an unattended living presence in a vehicle having at least two doors, comprising determining, before the vehicle starts moving, a first total number of vehicle door openings utilizing a non added-on door sensor integrated in the vehicle, each of the door sensors is associated with at least one of the at least two doors and is indicative of a door state, wherein each opening of a door indicates a change in a door state of a door, out of the at least two doors, from a door closed state to a door open state; determining, after the vehicle has stopped moving and until being locked, a second total number of vehicle door openings utilizing the non added-on door sensors; and in case the first total number exceeds the second total number, outputting an alert on a possible unattended living presence in a vehicle.
Abstract:
A system for instantaneous and continuous nanosecond-level accuracy determination of a relative time offset between at least two non-collocated timing units, the system comprising at least two non-collocated timing units located at known positions, each timing unit comprising a frequency source and a collocated receiver, each frequency source being disciplined at a frequency domain using a time source to generate corrections of the relative frequency drift between the frequency source and the time source.
Abstract:
A system for instantaneous and continuous nanosecond-level accuracy determination of a relative time offset between at least two non-collocated timing units, the system including at least two non-collocated timing units located at known positions, each timing unit comprising a frequency source and a collocated receiver, each frequency source being disciplined at a frequency domain using a time source to generate corrections of the relative frequency drift between the frequency source and the time source.
Abstract:
An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile.
Abstract:
A computer-implemented method for detecting an unattended living presence in a vehicle having at least two doors, comprising determining, before the vehicle starts moving, a first total number of vehicle door openings utilizing a non added-on door sensor integrated in the vehicle, each of the door sensors is associated with at least one of the at least two doors and is indicative of a door state, wherein each opening of a door indicates a change in a door state of a door, out of the at least two doors, from a door closed state to a door open state; determining, after the vehicle has stopped moving and until being locked, a second total number of vehicle door openings utilizing the non added-on door sensors; and in case the first total number exceeds the second total number, outputting an alert on a possible unattended living presence in a vehicle.
Abstract:
An exo-atmospheric intercepting method for intercepting in space multiple objects, including acquiring and tracking multiple inflated objects which fly towards a protected territory. The method further includes launching an interceptor missile accommodating a plurality of kill vehicles each hosting a plurality of punching objects and classifying the multiple objects into clusters. In respect of each cluster of objects, determining an ejection condition responsive to meeting of which a kill vehicle is ejected from the interceptor missile towards the cluster of objects and thereafter releasing from the kill vehicle a plurality of punching objects such that every inflated object in the cluster is likely, with a high degree of certainty, to be punched by one or more punching objects.
Abstract:
An exo-atmospheric intercepting method for intercepting in space multiple objects, including acquiring and tracking multiple inflated objects which fly towards a protected territory. The method further includes launching an interceptor missile accommodating a plurality of kill vehicles each hosting a plurality of punching objects and classifying the multiple objects into clusters. In respect of each cluster of objects, determining an ejection condition responsive to meeting of which a kill vehicle is ejected from the interceptor missile towards the cluster of objects and thereafter releasing from the kill vehicle a plurality of punching objects such that every inflated object in the cluster is likely, with a high degree of certainty, to be punched by one or more punching objects.
Abstract:
An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile
Abstract:
Method for providing a known reference point for an airborne imaging system, the method including providing at measured earth co-ordinates a camera/mirror assembly having a camera and a mirror mounted in fixed mutual spatial relationship and capable of tilting about two mutually orthogonal axes. Using the camera to track the sun and produce at least two or more different measured times respective time tagged camera images. Using the time tagged camera images to obtain a transformation of mirror axes relative to axes of the earth at a mirror location on the earth where the mirror is mounted.During a time window when the mirror is within a line of sight of the airborne imaging system and the sun, adjusting the azimuth and elevation of the mirror so that the sun is reflected by the mirror toward the airborne imaging system thereby capturing an image of the mirror in an aerial image produced by the airborne imaging system. Determining a location in the aerial image corresponding to the mirror thus providing a known earth reference location in said aerial image.