Compensating Non-Ideal Reflector Surfaces in Satellite Beamforming

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Solution Overview

Problem

Satellite communication systems face performance degradation due to non-ideal reflector surfaces, which cause unpredictable side-lobe performance and degrade carrier-to-interference (C/I) ratios, especially in larger reflectors with deployment-induced distortions.

Innovation Solution

The system measures signals reflected off a non-ideal reflector surface, calculates element correlation matrices from these measurements, and adjusts beam weights to form beams that mimic the performance of an ideal reflector surface, ensuring desired parameters like C/I ratios are met.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Length of moving object

If a large reflector is deployed to enable narrower spot beams and maximum frequency reuse, then beam forming capability is improved, but surface distortion occurs resulting in non-ideal surface performance

Engineering Contradiction:
Improvereflector diameterVSAvoidsurface accuracy
Core Design Contradiction:
Length of moving objectVSManufacturing precision

Solution Approach 1:

The patent applies parameter changes by measuring the actual reflector surface deviations and adjusting the beamforming weights to compensate for these deviations. The system characterizes the reflector surface accuracy parameters and uses these measurements to optimize the beamforming parameters, thereby maintaining performance despite surface imperfections

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent implements feedback by measuring signals reflected off the actual reflector surface and using these measurements to calculate element correlation matrices. This feedback loop allows the system to adjust beam weights based on actual performance data, compensating for surface distortions and maintaining optimal beamforming performance

Inventive Principle:
Principle #23Feedback

2Reliability

If beam weights are adjusted to compensate for non-ideal surface, then C/I ratio is improved, but system complexity increases

Engineering Contradiction:
Improvecarrier-to-interference ratioVSAvoidbeam weight adjustment system
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent uses feedback by measuring reflected signals and using these measurements to calculate element correlation matrices that guide beam weight adjustments. This measured feedback approach provides reliable C/I ratio improvement while keeping the complexity manageable through data-driven optimization

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent changes beamforming parameters (weights) based on measured reflector characteristics and element correlation matrices. By optimizing these parameters according to actual surface conditions, the system achieves improved reliability without requiring complex hardware modifications

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach compensates for the non-ideal surface by adjusting beam weights, maintaining or improving performance metrics such as C/I ratios, even with distorted reflectors, thereby maintaining reliable communication.

Implementation Method 1

A number of satellites are currently being developed that include a large reflector

Methodology Applied
Scientific EffectReflection: Reflection

Implementation Method 2

A beamformer is configured to adjust amplitudes and phases of signals to one or more antenna feed elements

Methodology Applied
Scientific EffectBeam forming:

Data Source

PatentEP2973855B1Compensating for a non-ideal surface of a reflector in a satellite communication system
Publication Date: 2020.01.22 THE BOEING CO
  • EP2973855B1 patent drawingFigure 1
  • EP2973855B1 patent drawingFigure 2
  • EP2973855B1 patent drawingFigure 3

AI summary

A method is provided that includes measuring amplitudes and phases of signals reflected off a reflector of a satellite, with the amplitudes and phases forming a first set of measurements. The method includes calculating an element correlation matrix as a function of the first set of measurements. The element correlation matrix represents a radiated feed element pattern off the reflector. And the method includes adjusting a formed beam pattern of a beamformer based on the element correlation matrix to thereby compensate for a non-ideal surface of the reflector.