초록 ▼

A distributed ground sensor threat detection system, which is an automated missile warning system designed to provide reliable, timely and accurate missile location information of shoulder-launched SAMs within the volume under surveillance by a network of sensors. Remote sensor nodes position in pro

A distributed ground sensor threat detection system, which is an automated missile warning system designed to provide reliable, timely and accurate missile location information of shoulder-launched SAMs within the volume under surveillance by a network of sensors. Remote sensor nodes position in proximity to an airport runway monitor the area between the nodes to locate threat missiles. Detection information from each remote sensor node is sent to a central processing node which processes the information to determine if a threat missile is launched against a commercial aircraft.

대표청구항 ▼

What is claimed is: 1. A distributed ground-based threat detection system for monitoring a launch and flight of a missile in proximity to a takeoff and landing path at an airfield comprising: (a) a sensor grid consisting of a set of remote sensor nodes positioned in the vicinity of said takeoff and

What is claimed is: 1. A distributed ground-based threat detection system for monitoring a launch and flight of a missile in proximity to a takeoff and landing path at an airfield comprising: (a) a sensor grid consisting of a set of remote sensor nodes positioned in the vicinity of said takeoff and landing path on one side of said takeoff and landing path, each of said remote sensor nodes including: (i) a plurality of EO (electro-optic) sensors each having a field of view for monitoring the launch and flight of said missile which is targeted at aircraft traveling along said takeoff and landing path, said EO sensors at each remote sensor node generating video data of the launch and flight of said missile; and (ii) a plurality of High-Speed Capture and Detect (HSCD) processors wherein each of said HSCD processor is connected to one of said EO sensors to receive said video data from said EO sensor connected thereto, said HSCD processor digitizing and processing said video data to determine when a plume of said missile is within the field of view of said EO sensor, said HSCD processor generating sightline data representing a line of sight from said EO sensor to the plume of said missile; (iii) a two-way microwave datalink located between said remote sensor nodes for signal transmission and communications between said remote sensor nodes, wherein said two-way microwave datalink has an operating frequency in the range of 7125 to 8400 MHz and an Ethernet interface which has a data rate of 100 Mb/sec, said microwave datalink providing for a two-way voice channel between said remote sensor nodes; and (b) a central processing node connected to each of said remote sensor nodes by a network link wherein each of said HSCD processors at each remote sensor node transfers said sightline data to said central processing node via said network link, said central processing node including: (i) a frame merge module for receiving said sightline data via said network link from each of HSCD processors at each of said remote sensor nodes wherein said frame merge module compares gps time stamps of said sightline data to ensure that synchronized pairs of video frame sightline data are output from said frame merge module; (ii) a sightline correlator for receiving said synchronized pairs of video frame sightline data from said frame merge module, said sightline correlator processing said sightline data to determine when the line of sight for one of a pair of EO sensors having overlapping field of views intersects with the line of sight for the other of said pair of EO sensors to provide a data point for said missile during the launch and flight of said missile; (ii) a multisensor tracker for receiving said data points from said sightline correlator, said multisensor tracker correlating and combining said data points to provide estimates of position, velocity and acceleration of said missile, and an enhanced threat declaration performance; and (iii) a threat declaration module for comparing track dynamics including said estimates of position, velocity and acceleration of said missiles with missile flight profiles to determine if said missile is a threat missile launched against one of said aircraft. 2. The distributed ground-based threat detection system of claim 1 wherein said threat declaration module provides a launch confirmed signal sent to a countermeasures system when said threat declaration module determines that said threat missile is being launched against said aircraft, said countermeasures system, responsive to said launch confirmed signal, triggering release of countermeasures by said aircraft under attack, or activating a ground-based countermeasure system to defeat the threat missile. 3. The distributed ground-based threat detection system of claim 1 wherein said multisensor tracker correlator comprises a Kalman filter with a state vector consisting of position, velocity and acceleration in Cartesian coordinates, wherein said Kalman filter generates said estimates of position, velocity and acceleration of said missile to provide said enhanced threat declaration performance. 4. The distributed ground-based threat detection system of claim 3 wherein the position, velocity and acceleration estimated by said Kalman filter is compared to said missile flight profiles to consistently produce threat declarations by said threat declaration module which occur within seconds after launch of said threat missile. 5. The distributed ground-based threat detection system of claim 1 wherein said set of remote sensor nodes are located and orientated in the vicinity of said takeoff and landing path such that a volume requiring surveillance is viewable by said EO sensors from at least two of said remote sensor nodes in the sensor grid, said volume requiring surveillance comprising a region surrounding said takeoff and landing path where said threat missile is within a lethal range of said aircraft when said aircraft is along said takeoff and landing path. 6. The distributed ground-based threat detection system of claim 1 wherein each of said HSCD processors accurately and consistently locate the plume of said missile within the field of view of said EO sensor connected thereto, while minimizing non-threat background clutter by looking for a high level of contrast between the plume of said missile and said non-threat background clutter and by looking for motion from the plume of said missile.