AESA Calibration Using Static Probe Far-Field Estimation

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Solution Overview

Problem

AESA radar systems are highly sensitive to small miscalibrations and require meticulous testing and calibration due to mechanical and electrical imperfections, which conventional far field and near field metrology methods are slow and cumbersome, involving large, electrically quiet enclosures and extensive mechanical rotations.

Innovation Solution

A Fast Array Test Environment (FATE) approach that uses a static mount, precision network analyzer, and test processor to evaluate RF amplitudes and phases without mechanical movement, allowing rapid calibration and validation of AESA systems by analyzing electronic parameter spaces.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If conventional far field and near field metrology methods are used for AESA calibration, then measurement precision is maintained, but testing time is excessively long and device complexity is high

Engineering Contradiction:
Improvecalibration accuracyVSAvoidtesting time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The patent replaces mechanical rotation systems with electronic beam steering. Instead of physically rotating the AESA or test probes through mechanical actuators, the system uses electronic phase control to steer radar beams in different directions. This substitution eliminates mechanical movement while maintaining the ability to perform comprehensive calibration measurements across all beam directions, dramatically reducing testing time while preserving measurement precision.

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

Solution Approach 2:

The patent implements preliminary characterization of individual antenna elements before performing array calibration. By first measuring and storing the radiation patterns and electrical characteristics of each element in isolation, the system prepares reference data that accelerates the subsequent array-level calibration process. This preliminary action eliminates the need for repeated individual element measurements during array calibration, significantly reducing total testing time.

Inventive Principle:
Principle #10Preliminary action

2Measurement precision

If conventional far field and near field metrology methods are used for AESA calibration, then measurement precision is maintained, but device complexity and enclosure requirements increase

Engineering Contradiction:
Improvecalibration accuracyVSAvoidtesting system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical rotation systems and large anechoic enclosures with electronic beam steering capabilities. The testing system uses software-controlled phase shifters to electronically steer beams without mechanical movement, eliminating the need for complex mechanical actuators, precision alignment mechanisms, and large physical enclosures. This reduces device complexity while maintaining calibration accuracy through consistent, repeatable electronic positioning.

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

Solution Approach 2:

The patent uses computational models and simulated far-field patterns derived from near-field measurements. Instead of requiring physical far-field measurement environments, the system creates computational copies of far-field radiation patterns through mathematical transformations of near-field data. This copying approach eliminates the need for large anechoic enclosures and complex mechanical positioning systems while preserving measurement accuracy.

Inventive Principle:
Principle #26Copying

3Reliability

If meticulous production testing is performed on AESA systems, then reliability is improved, but productivity decreases

Engineering Contradiction:
Improvesystem functionalityVSAvoidcalibration speed
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent performs preliminary characterization of individual antenna elements and stores their electrical characteristics in a database. This pre-characterization data includes radiation patterns, impedance values, and phase responses for each element. During production testing, the system retrieves this stored data and performs rapid array-level calibration by comparing actual measurements against the preliminary reference data, dramatically accelerating the calibration process while maintaining thoroughness and reliability.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent replaces time-consuming mechanical scanning and rotation procedures with electronic beam steering and computational analysis. The system uses software-controlled phase shifters to rapidly change beam directions without mechanical movement, and employs computational algorithms to analyze array performance. This electronic and computational approach performs meticulous calibration checks much faster than mechanical methods, improving productivity while maintaining reliability through comprehensive testing.

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

Data Source

PatentUS20260063696A1Fate factory calibration and test
Publication Date: 2026.03.05 ROCKWELL COLLINS INC
  • US20260063696A1 patent drawing
  • US20260063696A1 patent drawing
  • US20260063696A1 patent drawing

AI summary

A test system is presented for validating and calibrating an active electronically scanned array (AESA) with multiple distinct transceiver elements and associated RF channels. The test system includes a static mount for the AESA, and a test probe fixedly located relative to the static mount. The system also includes a network analyzer connected to the AESA and the test probe, and a test processor connected to the network analyzer. The network analyzer provides RF evaluations of amplitudes and phases/time delays to the test processor, which estimates far field (FF) patterns of the AESA based on these inputs and assessments of free space path losses and propagation delays between the AESA and the test probe. The test processor calculates FF figures of merit (FoMs) for the AESA as a function of frequency, beam scan, and environmentals based on the estimated FF patterns, and validates the AESA based on these FF FoMs.