Pulse Doppler radar with fixed target echo rejection circuit formed of recursion filters

Claim 2

A pulse Doppler radar with a range gate circuit and with a fixed target echo rejection circuit, consisting of recursion filters with at least one delay element which has a return loop wherein weighting of the recursion signals occurs and upon a change of the pulse repetition frequency (PRF) the weighting factors are changed by means of a weighting multiplier, characterized in that the switching of the weighting factors (a, b, c . . . ) corresponding to each pulse repetition frequency occurs at a delayed time after a change of the pulse repetition frequency at the time at which the recursion signal (A, B, C . . . ) which is returned from the output of the delay line passes through zero.

Claim 3

A pulse Doppler radar with a range gate circuit and with a fixed target echo rejection circuit, consisting of recursion filters with at least one delay element which has a return loop wherein weighting of the recursion signals occurs and upon a change of the pulse repetition frequency (PRF) the weighting factors are changed by means of a weighting multiplier, characterized in that the switching of the weighting factors (a, b, c . . . ) corresponding to each pulse repetition frequency occurs at a delayed time after a change of the pulse repetition frequency at the time at which the recursion signal (A, B, C . . . ) which is returned from the output of the delay line passes through zero, and characterized in that the delayed switching of the weighting factor for a recursion filter constructed in analog technology occurs by using a zero detector (window discriminator) in conjunction with a D-flip-flop, and said zero detector being connected to the signal input of the weighting multiplier (WM).

Claim 4

A pulse Doppler radar with a range gate circuit and with a fixed target echo rejection circuit, consisting of recursion filters with at least one delay element which has a return loop wherein weighting of the recursion signals occurs and upon a change of the pulse repetition frequency (PRF) the weighting factors are changed by means of a weighting multiplier, characterized in that the switching of the weighting factors (a, b, c . . . ) corresponding to each pulse repetition frequency occurs at a delayed time after a change of the pulse repetition frequency at the time at which the recursion signal (A, B, C . . . ) which is returned from the output of the delay line passes through zero, and characterized in that the delayed switching of the weighting factor for a recursion filter constructed in analog technology occurs by using a zero detector (window discriminator) in conjunction with a D-flip-flop, and said zero detector being connected to the signal input of the weighting multiplier (WM).

Claim 5

A pulse Doppler radar with a range gate circuit and with a fixed target echo rejection circuit, consisting of recursion filters with at least one delay element which has a return loop wherein weighting of the recursion signals occurs and upon a change of the pulse repetition frequency (PRF) the weighting factors are changed by means of a weighting multiplier, characterized in that the switching of the weighting factors (a, b, c . . . ) corresponding to each pulse repetition frequency occurs at a delayed time after a change of the pulse repetition frequency at the time at which the recursion signal (A, B, C . . . ) which is returned from the output of the delay line passes through zero, characterized in that the delayed switching of the weighting factor for an analog recursion filter occurs by using employment of a zero comparator connected to the signal output of the weighting multiplier (WM), and said zero comparator being connected to a D-flip-flip through a differentiation circuit and a double path rectifier circuit.

Claim 6

A pulse Doppler radar with a range gate circuit and with a fixed target echo rejection circuit, consisting of recursion filters with at least one delay element which has a return loop wherein weighting of the recursion signals occurs and upon a change of the pulse repetition frequency (PRF) the weighting factors are changed by means of a weighting multiplier, characterized in that the switching of the weighting factors (a, b, c . . . ) corresponding to each pulse repetition frequency occurs at a delayed time after a change of the pulse repetition frequency at the time at which the recursion signal (A, B, C . . . ) which is returned from the output of the delay line passes through zero, characterized in that the delayed switching of the weighting factor for an analog recursion filter occurs by using employment of a zero comparator connected to the signal output of the weighting multiplier (WM), and said zero comparator being connected to a D-flip-flip through a differentiation circuit and a double path rectifier circuit.

Claim 7

A pulse Doppler radar with a range gate circuit and with a fixed target echo rejection circuit, consisting of recursion filters with at least one delay element which has a return loop wherein weighting of the recursion signals occurs and upon a change of the pulse repetition frequency (PRF) the weighting factors are changed by means of a weighting multiplier, characterized in that the switching of the weighting factors (a, b, c . . . ) corresponding to each pulse repetition frequency occurs at a delayed time after a change of the pulse repetition frequency at the time at which the recursion signal (A, B, C . . . ) which is returned from the output of the delay line passes through zero, and characterized in that the delayed switching of the weighting factor switching with a digital recursion filter, the operational sign of the digital signals at the input and output of each delay element (shift register) are monitored by an exclusion OR gate and are evaluated in conjunction with a D-flip-flop.

Claim 8

A pulse Doppler radar with a range gate circuit and with a fixed target echo rejection circuit, consisting of recursion filters with at least one delay element which has a return loop wherein weighting of the recursion signals occurs and upon a change of the pulse repetition frequency (PRF) the weighting factors are changed by means of a weighting multiplier, characterized in that the switching of the weighting factors (a, b, c . . . ) corresponding to each pulse repetition frequency occurs at a delayed time after a change of the pulse repetition frequency at the time at which the recursion signal (A, B, C . . . ) which is returned from the output of the delay line passes through zero, and characterized in that the delayed switching of the weighting factor switching with a digital recursion filter, the operational sign of the digital signals at the input and output of each delay element (shift register) are monitored by an exclusion OR gate and are evaluated in conjunction with a D-flip-flop.

Claim 9

A pulse Doppler radar with a range gate circuit and a fixed target echo rejection circuit comprising a sample-and-hold circuit which receives an input signal, a variable pulse repetition frequency oscillator supplying an input to said sample-and-hold circuit, a frequency selector logic circuit connected to said pulse repetition frequency oscillator, a summing circuit receiving the output of said sample-and-hold circuit, a first delay element receiving the output of said summing circuit, a zero crossing detector connected to the output of said first delay element, a first flip-flop circuit receiving inputs from said zero crossing detector and said frequency selector logic circuit, a first source of weighting multiplier factors and said first flip-flop circuit connected to control the output weighting factor, and a first weighting multiplier receiving the outputs of said first delay element and said first source of weighting multiplier factors and supplying an output to said summing circuit.

Claim 10

A pulse Doppler radar with a range gate circuit and a fixed target echo rejection circuit comprising a sample-and-hold circuit which receives an input signal, a variable pulse repetition frequency oscillator supplying an input to said sample-and-hold circuit, a frequency selector logic circuit connected to said pulse repetition frequency oscillator, a summing circuit receiving the output of said sample-and-hold circuit, a first delay element receiving the output of said summing circuit, a zero crossing detector connected to the output of said first delay element, a first flip-flop circuit receiving inputs from said zero crossing detector and said frequency selector logic circuit, a first source of weighting multiplier factors and said first flip-flop circuit connected to control the output weighting factor, and a first weighting multiplier receiving the outputs of said first delay element and said first source of weighting multiplier factors and supplying an output to said summing circuit.

Claim 11

A pulse Doppler radar according to claim 5 wherein said zero crossing detector comprises a window discriminator.

Claim 12

A pulse Doppler radar according to claim 5 wherein said zero crossing detector comprises, a comparator, a differentiator connected to the output of said comparator and a dual path rectifier connected to the output of said differentiator.

Claim 13

A pulse Doppler radar according to claim 5 wherein said zero crossing detector comprises an exclusive OR gate connected across the input and output of said first delay element and supplying an input to said first flip-flop circuit.

Claim 14

A pulse Doppler radar according to claim 5 including a second delay element connected to the output of said first delay element, a second zero crossing detector connected to the output of said second delay element, a second flip-flop receiving inputs from said second zero crossing detector and said frequency selector logic circuit, a second source of weighting multiplier factors and said second flip-flop connected to control the output weighting factor, a second weighting multiplier receiving the outputs of said second delay element and said second source of weighting factors and supplying an output to said summing circuit.