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AssigneeHughes Aircraft Company
InventorsLaurence E. Broniwitz, Mark I. Landau, John B. Pearson, III
Estimating the term…
A pulse-doppler radar tracking system is disclosed employing four filter channels for tracking range, velocity, azimuth and elevation. Each channel is mechanized in a Kalman filter form by a stored program in a digital computer. The range channel estimates target range, R.sub.TPR, range rate, V.sub.TPV and acceleration a.sub.TPV from one of many received signal frequency spectra at multiples of the pulse repetition frequency (PRF). Once error in the range rate estimate, V.sub.TPR, is within a velocity corresponding to .lambda. PRF/4, the velocity channel is reinitialized in its estimate of target velocity, V.sub.TPV, with a corrected velocity computed from the less accurate but unambiguous estimate of velocity, V.sub.TPR, and the ambiguous estimate of velocity, V.sub.TPV.
In a radar system for tracking a target aircraft, said system having antenna for cyclically sensing reflected electromagnetic energy from said target at a particular pulse repetition frequency, PRF, and wavelength, .lambda., and producing signals representing discriminants .DELTA.R.sub.m and .DELTA.V.sub.m of range and radial velocity, respectively, of said target relative to said tracking system, where said velocity discriminants are derived from doppler shift measurements, a separate filter for tracking target range and velocity, each filter responding to respective discriminants .DELTA.R.sub.m and .DELTA.V.sub.m to generate predictions of the next measurements from current estimates of filter states, where the states are vectors X.sub.R (i) and X.sub.V (i), and the subscript i indicates a value of time i, a method for resolving ambiguity of said vector X.sub.V (i) after a period of initial tracking sufficient for said range tracking filter to unambiguously achieve an accuracy in current estimates of states in said range filter for the difference between the first derivative of the range value in X.sub.R (i) effectively estimated as one of said range filter states, and the true doppler velocity to be a velocity less than .lambda.PRF/4, said method being performed by computer means for computing a corrected target velocity V.sub.TCORR from doppler shift information in accordance with the equation ##EQU43## by the steps of determining f.sub.MLC as an offset in a doppler shift spectra reference introduced to avoid main lobe clutter in the center of a doppler shift spectrum where the true target return is likely to be, f.sub.DAP as the ambiguous doppler shift measurement derived from an ambiguous velocity estimate X.sub.V (i), and f.sub.DP as actual doppler shift estimate derived as the estimate of the first derivative of the unambiguous velocity in X.sub.R (i), truncating the bracketed quantity as indicated by the asterisk by dropping the fractional part thereof of the bracketed quantity after the quotient of (f.sub.MLC +f.sub.DAP -f.sub.DP) is divided by PRF and has been rounded by adding 1/2 to the quotient and subtracting (f.sub.DAP +f.sub.MCL) from the bracketed quantity and multiplying the difference by .lambda./2 PRF.
In a radar system for tracking a target aircraft, said system having antenna for cyclically sensing reflected electromagnetic energy from said target at a particular pulse repetition frequency, PRF, and wavelength, .lambda., and producing signals representing discriminants .DELTA.R.sub.m and .DELTA.V.sub.m of range and radial velocity, respectively, of said target relative to said tracking system, where said velocity discriminants are derived from doppler shift measurements, a separate filter for tracking target range and velocity, each filter responding to respective discriminants .DELTA.R.sub.m and .DELTA.V.sub.m to generate predictions of the next measurements from current estimates of filter states, where the states are vectors X.sub.R (i) and X.sub.V (i), and the subscript i indicates a value at time i, apparatus for resolving ambiguity of said vector X.sub.V (i) after a period of initial tracking sufficient for said range tracking filter to unambiguously achieve an accuracy in current estimates of states in said range filter for the difference between the first derivative of the range value in X.sub.R (i) effectively estimated as one of said range filter states, and the true doppler velocity to be a velocity less than .lambda.PRF/4, said apparatus being comprised of computer means for computing a corrected target velocity V.sub.TCORR from doppler shift information in accordance with the equation ##EQU44## where f.sub.MLC is an offset in a doppler shift spectra reference introduced to avoid main lobe clutter in the center of a doppler shift spectrum where the true target return is likely to be, f.sub.DAP is the ambiguous doppler shift measurement derived from an ambiguous velocity estimate X.sub.V (i), f.sub.DP is actual doppler shift estimate derived as the estimate of the first derivative of the unambiguous velocity in X.sub.R (i), and the asterisk indicates the bracketed quantity is truncated by dropping the fractional part thereof after the quotient of (f.sub.MLC +f.sub.DAP -f.sub.DP) is divided by PRF and has been rounded by adding 1/2 to the quotient.
In a radar system for tracking a target aircraft, said system having antenna means for cyclically sensing reflected electromagnetic energy from said target at a particular pulse repetition frequency, PRF, and wavelength, .lambda., a separate filter for tracking target range and velocity, each filter generating predictions of the next measurements from current estimates of filter states, apparatus comprising computer means for computing a corrected target velocity V.sub.TCORR from doppler shift information in accordance with the equation ##EQU45## where f.sub.MLC is an offset in a doppler shift spectra reference introduced to avoid main lobe clutter in the doppler shift spectrum where the true target return is likely to be, f.sub.DAP is the ambiguous doppler shift measurement derived from an ambiguous velocity, and f.sub.DP is a doppler shift estimate range, and the asterisk indicates the bracketed quantity is truncated by dropping the fractional part thereof after the quotient of (f.sub.MLC +f.sub.DAP -f.sub.DP) is divided by PRF and has been rounded by adding 1/2 to the quotient.
In a pulse doppler radar system operable to transmit a signal at a selected pulse PRF and a signal .lambda. for tracking a target, a system for resolving velocity ambiguity of an ambiguous target spectral line in a plurality of PRF regions comprising:
Dependencies are inferred from the claim text.