Tracking system utilizing Kalman filter concepts

In an airborne system having direction sensitive means for cyclically sensing electromagnetic energy from a target and producing pulse signals proportional thereto for tracking moving targets, the combination comprising

• means connected to said sensing means and responsive to said energy received from said target for cyclically developing signals representing discriminants of at least elevation, .DELTA..epsilon..sub.m, and azimuth, .DELTA..eta..sub.m ;
• means responsive to said signals representing discriminants for cyclically generating predictions of the next measurements of elevation, X.sub.e, and azimuth, X.sub.d, from current estimates of tracking system vectors, using for each vector an equation of the general form
• X.sub.i.sub.+1 = .PHI..sub.i X.sub.i + L.sub.i + K.sub.i (Y.sub.i -H.sub.i X.sub.i)
• where X is a multistate vector, .PHI. is a transition matrix, L is a vector of dynamical aiding terms to compensate for motion of said sensing means, K is a system gain factor, Y is the output of a measurement structure for said system, and H is the scaling factor which accounts for a system measurement parameter, where a bar over a symbol indicates a matrix quantity used in said tracking system as the system's version of the parameter represented by the symbol, the subscript i indicates a value during the ith cycle of iterative computations, and where X for respective elevation, e, and azimuth, d, tracking is
• .epsilon..sub.P.sbsb.e .epsilon..sub.P.sbsb.d .omega..sub.LSP.sbsb.e .omega..sub.LSP.sbsb.d X.sub.e = a.sub.T.sbsb.d X.sub.d = a.sub.T.sbsb.e S.sub.e S.sub.d thus generating estimates of pointing errors .epsilon..sub.e and .epsilon..sub.d, target line-of-sight rates, .omega..sub.LSP.sbsb.e and .omega..sub.LSP.sbsb.d, target accelerations normal to the line-of-sight, a.sub.T.sbsb.d and a.sub.T.sbsb.e, and target angular scintillations, S.sub.e and S.sub.d, all referenced directly to antenna coordinates, the subscript P designating a prediction,
• means responsive to states of said tracking vectors for producing tracking commands, and
• means responsive to said commands for driving said system, thereby tracking said target.

In a monopulse radar tracking system having a direction sensitive antenna for cyclically sensing reflected electromagnetic energy from a moving target and producing signals .DELTA.R.sub.m, .DELTA.V.sub.m, .DELTA..epsilon..sub.m and .DELTA..eta..sub.m representing discriminants of elevation, azimuth, range and radial velocity, respectively, of said target relative to said tracking system, filters for tracking target range, velocity, elevation and azimuth, each filter responding to respective discriminants .DELTA.R.sub.m, .DELTA.V.sub.m, .DELTA..epsilon..sub.m and .DELTA..eta..sub.m to generate predictions of the next measurements from current estimates of filter states, where the states are vectors [X.sub.R (i), X.sub.V (i), X.sub.e (i) and X.sub.d (i),] X.sub.R (i), X.sub.V (i), X.sub.e (i) and X.sub.d (i), using for each state an equation of the general form

• X.sub.i.sub.+1 = .PHI..sub.i X.sub.i + K.sub.i (Y.sub.i - H.sub.i X.sub.i)
• where X is a state vector, .PHI. is a transition matrix, K is a gain factor, Y is the output of a measurement structure for the dynamical system, H is a system scaling factor which accounts for the gain in the measurement structure, a over X indicates the estimate of X, a bar over a symbol indicates a matrix quantity or value used in the filter for the parameter represented by the symbol, and the subscript i indicates a value at time i while the subscript i+1 indicates a value at the next iteration time.