IP Library Granted Patent US 7,218,269
Granted Patent B2
US 7,218,269 · App. 10/830,776 · Granted May 15, 2007

Method for enlarging the interference-free dynamic range of non-linear signal processing components

Assignee: EADS Deutschland GmbH
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Quick Facts
Patent No.
US 7,218,269
App. No.
10/830,776
Granted
May 15, 2007
Kind
B2
Abstract

A method for enlarging the interference-free dynamic range of non-linear signal-processing components in receiver systems, in the conversion of input frequencies f in into output frequencies f out . According to the invention, at least one linear combination of at least one input frequency f in,t , f in,b and a fixed, predetermined oscillator f LOn of the components is calculated from the output signal of the component, for at least one output frequency f out,s , f out1,s , f outs,2 , which combination is compared with any desired output frequency f out,t of the component, whereby the output frequency f out,s , f out1,s , f outs,2 is then recognized as a spur and eliminated from the output signal of the component, if the calculated linear combination corresponds to any desired output frequency f out,t of the component, within a frequency and power range that can be predetermined.

Claims (142)

1. A method for enlarging an interference-free dynamic range of non-linear signal-processing components in receiver systems, in the conversion of input frequencies f in into output frequencies f out , comprising:

calculating at least one linear combination of at least one input frequency f in,t , f in,b and a fixed, predetermined oscillator f LOn of the components from an output signal of the component, for at least one output frequency f out,s , f out1,s , f outs,2 ;

comparing said combination with any desired output frequency f out,t of the component;

recognizing an output frequency f out,s , f out1,s , f outs,2 as a spur; and

eliminating said output frequency recognized as a spur from the output signal of the component, if the calculated linear combination corresponds to any desired output frequency f out,t of the component, within a predetermined frequency and power range.

2. A method according to claim 1 , wherein the output frequencies f out,s , f out1,s , f outs,2 to be checked are sorted in the output signal according to their power, in ascending or descending order.

3. A method according to claim 1 , wherein the linear combination that can be predetermined is a linear combination of mixer harmonics.

4. A method according to claim 2 , wherein the original input frequency f in,b ahead of a signal-processing, non-linear component is calculated for each output frequency f out,s of the output signal to be checked.

5. A method according to claim 4 , wherein linear combinations are calculated for the output frequency f out,s according to

f

out

,

s

z

=

A

·

f

i

n

,

b

+

n

=

1

N

B

n

·

f

LOn

with

A, B n : parameters that can be predetermined, with A, B n εZ,

f in,b : input frequency ahead of the non-linear component,

f LOn oscillator frequency of an n th stage of the non-linear component,

N: number of stages,

z: running variable of the calculated linear combination.

6. A method according to claim 2 , wherein the linear combination that can be predetermined is a linear combination of intermodulations.

7. A method according to claim 6 , wherein the output frequency f out,b is calculated with a linear combination according to

f

out

,

b

z

=

C

A

f

i

n1

,

s

+

n

=

1

M

x

(

n

)

·

f

LOn

±

B

f

i

n2

,

s

+

n

=

1

M

x

(

n

)

·

f

LOn

+

n

=

M

+

1

N

x

(

n

)

·

f

LOn

with

A, B, C: parameters that can be predetermined, with A, BεZ,

f in1,s : first input signal ahead of the component,

f in2,s : second input signal ahead of the component,

f LOn : oscillator frequency of an n th stage of the non-linear component,

N: number of stages of the non-linear component,

M: position of the non-linear component to be checked,

x(n): function that can be predetermined, with values +1 and −1,

z: running variable of the calculated linear combination.

Assignments (2)
CHANGE OF NAME Recorded Jan 6, 2017
From: EADS DEUTSCHLAND GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 041292/0613 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 30, 2004
From: GOTTSCHEBER, HOLGER
To: EADS DEUTSCHLAND GMBH
Reel/Frame 015736/0559 →
Priority Claims (1)
DE 103 18 754 · Apr 25, 2003 · national
Continuity (1)
Related Publication 20040263384A1 · Dec 30, 2004