초록 ▼

Methods are disclosed for obtaining a cued radar acquisition volume. The method employs uncertainties (i.e., errors) represented by a covariance, and a method of finding the minimum volume defined by range, azimuth, and elevation limits that enclose the covariance, and uses a perspective projection

Methods are disclosed for obtaining a cued radar acquisition volume. The method employs uncertainties (i.e., errors) represented by a covariance, and a method of finding the minimum volume defined by range, azimuth, and elevation limits that enclose the covariance, and uses a perspective projection of the errors to provide an accurate calculation of the cued acquisition volume. The three-dimensional problem is first reduced to two dimensions by parallel projection onto the range-transverse and range-elevation planes. Then perspective projection of the two dimensional parallel projections is performed. The disclosed method reduces the complexity of three dimensional perspective projection by preceding perspective projection with parallel projection, which greatly simplifies the problem and allows a simple and easily calculated solution.

대표청구항 ▼

1. A method for generating a radar search volume enclosing a tracked target, the method comprising: parallel projecting a three-dimensional covariance of the tracked target onto a range-transverse plane and a range-elevation plane to obtain two-dimensional covariances;determining, by a command and d

1. A method for generating a radar search volume enclosing a tracked target, the method comprising: parallel projecting a three-dimensional covariance of the tracked target onto a range-transverse plane and a range-elevation plane to obtain two-dimensional covariances;determining, by a command and decision processor, an average elevation extent and average azimuth extent by perspective projecting the two-dimensional covariances;andgenerating the search volume using the average elevation extent and the average azimuth extent. 2. The method according to claim 1, wherein determining the average elevation extent and the average azimuth extent by perspective projecting the two-dimensional covariances comprises: generating, by the command and decision processor, an error ellipsecorresponding to each of the two-dimensional covariances;determining, by the command and decision processor, a point of tangency on each of the error ellipses;determining, by the command and decision processor, maximum elevation and transverse extents of the search volume using the points of tangency; anddetermining, by the command and decision processor, an average elevation extent and an average azimuth extent from the maximum elevation and transverse extents. 3. The method according to claim 2, wherein determining, by the command and decision processor, the point of tangency on each of the error ellipses comprises using a tangent formula for a geometric figure and simultaneously solving, for each error ellipse, an equation for a line containing the point of tangency and a coordinate origin, and an equation for the error ellipse containing the point of tangency. 4. The method according to claim 2, wherein determining, by the command and decision processor, the maximum elevation and transverse extents of the search volume from the points of tangency comprises determining the maximum elevation and transverse extents of the search volume using the inverse tangent of a ratio of the coordinates of the points of tangency. 5. The method according to claim 1, further comprising receiving, by a communications unit, tracking data relating to the tracked target from a remote radar system. 6. The method according to claim 5, wherein the tracking data received by the communications unit from the remote radar system is transformed into coordinates of a local radar system generating the radar search volume, prior to parallel projecting of the three-dimensional covariance of the tracked target. 7. The method according to claim 1, further comprising determining, by the command and decision processor, an elevation center for an acquisition face of the search volume based on the average elevation extent and a nominal elevation of the target and determining an azimuth center for the acquisition face of the search volume based on the average azimuth extent and a nominal azimuth of the target. 8. A radar system for generating a radar search volume enclosing a tracked target, the radar system comprising: a command and decision unit configured to: parallel project a three-dimensional covariance of the tracked target onto a range-transverse plane and a range-elevation plane to obtain two-dimensional covariances;determine an average elevation extent and average azimuth extent by perspective projecting the two-dimensional covariances;anda radar beam controller configured to generate the search volume using the average elevation extent and the average azimuth extent. 9. The radar system of claim 8, wherein the command and decision unit being configured to determine the average elevation extent and the average azimuth extent by perspective projecting the two-dimensional covariances comprises the command and decision unit being configured to: generate an error ellipse corresponding to each of the two-dimensional covariances;determine a point of tangency on each of the error ellipses;determine maximum elevation and transverse extents of a search volume using the points of tangency; anddetermine an average elevation extent and an average azimuth extent from the maximum elevation and transverse extents. 10. The radar system of claim 9, wherein the command and decision unit being configured to determine the maximum elevation and transverse extents of the search volume using the points of tangency comprises the command and decision unit being configured to determine the maximum elevation and transverse extents of the search volume using the inverse tangent of a ratio of the coordinates of the points of tangency. 11. The radar system according to claim 9, wherein the command and decision unit being configured to determine the point of tangency on each of the error ellipses comprises the command and decision unit being configured to use a tangent formula for a geometric figure and simultaneously solve, for each error ellipse, an equation for a line containing the point of tangency and a coordinate origin, and an equation for the error ellipse containing the point of tangency. 12. The radar system according to claim 8, further comprising a communications unit configured to receive tracking data relating to the tracked target from a remote radar system. 13. The method according to claim 12, further comprising transforming, by the command and decision unit, the tracking data received from the remote radar system into coordinates of the radar system, prior to parallel projecting of the three-dimensional covariance of the tracked target. 14. The method according to claim 1, further comprising determining, by the command and decision unit, an elevation center for an acquisition face of the search volume based on the average elevation extent and a nominal elevation of the target and determining, by the command and decision unit, an azimuth center for the acquisition face of the search volume based on the average azimuth extent and a nominal azimuth of the target.