Elevation Null Command Generator for Monopulse Radar

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Solution Overview

Problem

Existing terrain following-terrain avoidance radars face accuracy issues due to bias effects from strong targets off the monopulse null, which are exacerbated by the need to maintain signal-to-noise ratio, limiting the system's ability to accurately direct the elevation monopulse null plane.

Innovation Solution

The elevation null command generator processes sum and difference channel outputs through multiple pairs of range gates spaced above and below a central range gate, cross-multiplying signals to isolate the elevation monopulse null direction independently of terrain backscatter, thereby improving pointing accuracy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a single range gate generator is used to stabilize the elevation monopulse null, then the system can maintain operation, but the accuracy is reduced due to bias effects from strong targets off the monopulse null

Engineering Contradiction:
Improveelevation pointing accuracyVSAvoidbias effects from strong targets
Core Design Contradiction:
Measurement precisionVSObject-affected harmful factors

Solution Approach 1:

The single range gate is divided into multiple range gates (first range gate, second range gate, third range gate, etc.) spaced at different time delays. Each range gate processes signals from different spatial regions, allowing the system to segment the terrain backscatter analysis and eliminate bias effects from strong off-null targets through comparative processing.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces an intermediary processing system that receives signals from multiple range gates and performs comparative analysis. This intermediary processing eliminates the direct harmful influence of strong off-null targets by using the multiple gated signals to compute a stabilized elevation monopulse null reference that is immune to such bias effects.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Object-affected harmful factors

If the time width of the range gate is narrowed to reduce bias effects, then the bias from off-null targets decreases, but the signal to noise ratio decreases, again impairing accuracy

Engineering Contradiction:
Improvebias effects from strong targetsVSAvoidsignal to noise ratio
Core Design Contradiction:
Object-affected harmful factorsVSMeasurement precision

Solution Approach 1:

The patent merges the outputs of multiple range gates through a processing system that combines the signals from the first, second, third and subsequent range gates. This merging process maintains a high effective signal-to-noise ratio by aggregating energy from multiple gates while simultaneously eliminating bias effects through the comparative processing architecture.

Inventive Principle:
Principle #5Merging (Combining)

3Measurement precision

If multiple pairs of range gates are used with cross-multiplication processing, then the elevation monopulse null direction can be isolated independently of terrain backscatter, but the device complexity increases

Engineering Contradiction:
Improveelevation monopulse null direction accuracyVSAvoidrange gate processing circuitry
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical or hardware-based terrain compensation mechanisms with an electronic signal processing approach. By using multiple range gates and electronic cross-multiplication processing, the system achieves independent isolation of the elevation monopulse null direction from terrain backscatter effects without requiring additional mechanical components or complex physical systems.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS8004453B1Elevation null command generator for monopulse radar airborne missile guidance systems
Publication Date: 2011.08.23 RAYTHEON CO
  • US8004453B1 patent drawing
  • US8004453B1 patent drawing
  • US8004453B1 patent drawing

AI summary

There is disclosed an elevation null command generator (ENCG) for use in airborne monopulse radar, and a novel missile guidance system made possible by use of the ENGC. The ENCG provides an accurate means of directing the elevation monopulse plane of a radar antenna at a patch of ground defined by a range signal generated within the radar or its associated equipment. It is shown that within the system range can define the elevation angle of concern. The ENCG includes a central range gate centered at the command range and a plurality of pairs of range gates, the two gates of each pair being time spaced before and after the central range gate, and has circuit means for normalizing the output of the range gates to eliminate the bias effects of strong targets adjacent to the monopulse null plane and ground surface intersection.