초록 ▼

A method for obtaining a sky view of a battle site, comprising launching an interceptor (2) towards at least one detected flying threat (3); the interceptor (2) tracking the threat (3) using at least one remote sensor for achieving a kill of the threat (3) at a designated kill site (4) being at a la

A method for obtaining a sky view of a battle site, comprising launching an interceptor (2) towards at least one detected flying threat (3); the interceptor (2) tracking the threat (3) using at least one remote sensor for achieving a kill of the threat (3) at a designated kill site (4) being at a large range from the at least one sensor; when the interceptor (2) approaches the kill site (4), releasing from the interceptor (2) at least one detachable vehicle (7) that includes at least one local sensor (8) for sensing the kill site (4) from a range considerably shorter than the large range and communicating the sensed data.

대표청구항 ▼

The invention claimed is: 1. A method for obtaining a sky view of a battle site, comprising, a) launching an interceptor missile toward at least one detected flying threat; b) tracking the at least one detected flying threat using at least one remote sensor, the interceptor missile configured to ac

The invention claimed is: 1. A method for obtaining a sky view of a battle site, comprising, a) launching an interceptor missile toward at least one detected flying threat; b) tracking the at least one detected flying threat using at least one remote sensor, the interceptor missile configured to achieve a kill of the at least one detected flying threat at a designated aerial kill site at a large range from the at least one remote sensor; c) releasing from the interceptor missile, when the interceptor missile approaches the kill site, at least one detachable vehicle comprising at least one guidable local sensor configured to sense, within a basket sphere, the aerial kill site from a range shorter than the large range; and d) communicating the sensed data, wherein from any point in the basket sphere the at least one guidable local sensor is capable of sensing the aerial kill site and the basket sphere is determined based upon a threat flying trajectory and an interceptor missile flying trajectory. 2. The method according to claim 1, wherein the flying threat is a ground-to-ground missile. 3. The method according to claim 2, wherein the ground-to-ground missile is of the “Scud” series. 4. The method according to claim 1, wherein the interceptor missile is of the “Arrow” series. 5. The method according to claim 1, wherein at least one of the local sensors is an image acquisition device, and the method further comprises acquiring a succession of images of the kill site and transmitting at least one of the images through a communication channel. 6. The method according to claim 5, wherein the image acquisition device is a video camera. 7. The method according to claim 6, wherein the detachable vehicle comprises a propelling system associated with a guidance system, and the method further comprises steering the at least one video camera for acquiring images of the kill site. 8. The method according to claim 1, wherein the detachable vehicle comprises a propelling system associated with a guidance system, and the method further comprises steering the at least one guidable local sensor substantially toward the kill site. 9. The method according to claim 1, wherein the detachable vehicle comprises at least two image acquisition devices, and the method further comprises determining a field of view, respective to each of the acquisition devices, each field of view being a predetermined field of view respective to each of the acquisition devices; acquiring a succession of images, using each of the at least two acquisition devices, at the predetermined field of view respective to each of the acquisition devices, and transmitting at least one of the images through a communication channel, for constructing a consolidated view of the kill site. 10. The method according to claim 9, wherein each of the at least two image acquisition devices is a video camera. 11. The method according to claim 1, further comprising receiving the sensed data, for constructing a high resolution view of the battle site. 12. A method for obtaining a sky view of an event site, comprising: a) launching an interceptor missile toward at least one detected threat; and b) the interceptor missile tracking the at least one detected threat, the interceptor missile comprising at least one detachable vehicle comprising at least one guidable local sensor configured to sense the event and to communicate the sensed data, and wherein the tracking uses at least one remote sensor for achieving a kill of the threat at a designated kill site, where the event site is different than the kill site. 13. The method according to claim 12, wherein the event site includes a fireball of an encounter between a previous threat and the interceptor missile. 14. A device for obtaining a sky view of a battle site, the device comprising: an interceptor missile configured to be launched toward at least one detected flying threat and to track the at least one detected flying threat using at least one remote sensor for achieving a kill of the at least one detected flying threat at a designated aerial kill site at a large range from the at least one remote sensor, based on a threat flying trajectory and an interceptor missile flying trajectory; and a vehicle detachable from the interceptor missile, the vehicle is releasable from the interceptor missile upon approaching the aerial kill site, the vehicle comprising: at least one guidable local sensor configured to sense, within a basket sphere, the aerial kill site from a range shorter than the large range and configured to generate digital data indicative thereof, wherein from any point in the basket sphere the at least one guidable local sensor is capable of sensing the aerial kill site and the basket sphere is determined based upon the threat flying trajectory and the interceptor missile flying trajectory; and communication means configured to communicate the sensed data. 15. The device according to claim 14, wherein at least one of the guidable local sensors is an image acquisition device configured to acquire a succession of images of the kill scene, and the communication means are configured to transmit at least one of the images. 16. The device according to claim 15, wherein the image acquisition device is a video camera. 17. The device according to claim 16, wherein the detachable vehicle comprises a propelling system associated with a guidance system configured to steer the at least one guidable local sensor substantially toward the kill site. 18. The device according to claim 16, wherein the detachable vehicle comprises a propelling system associated with guidance system configured to steer the at least one video camera for acquiring images of the kill site. 19. The device according to claim 14, wherein the detachable vehicle comprises at least two image acquisition devices; each one of the acquisition devices is configured to acquire a succession of images at a respective predetermined field of view, the communication means are configured to transmit at least one of the images, whereby a consolidated view of the kill site can be constructed.