Imaging Array Fed Reflector Antenna Design

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Solution Overview

Problem

Conventional multi-beam antenna systems for spacecraft face inefficiencies due to shared radiating elements, requiring multi-carrier operation which leads to amplifier output back-off, reduced efficiency, and increased power and heat generation, or necessitate higher power amplifiers and redundancy, resulting in higher cost and complexity, while being scan limited by reflector offset distortion.

Innovation Solution

A multi-beam antenna system utilizing an imaging array fed reflector with dedicated clusters of radiating elements and power amplifiers for each beam, arranged in a close-packed triangular lattice, eliminating element sharing and employing gallium nitride solid-state power amplifiers to minimize line losses and reduce component complexity, with soft redundancy and Doherty amplifier configurations for improved efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If shared radiating elements are used between multiple beams, then device complexity is reduced, but beam forming efficiency deteriorates and multi-carrier operation is required leading to amplifier output back-off and reduced amplifier efficiency

Engineering Contradiction:
Improveantenna structure complexityVSAvoidbeam forming efficiency
Core Design Contradiction:
Device complexityVSProductivity

Solution Approach 1:

The antenna system divides the radiating elements into dedicated clusters, where each cluster is assigned to a specific beam. This segmentation eliminates element sharing between beams, allowing each beam to have its own dedicated radiating elements and power amplifiers, thereby improving beam forming efficiency without significantly increasing overall system complexity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent transitions from a conventional 2D planar array to a 3D volumetric arrangement of radiating elements distributed throughout a reflective volume. This dimensional change enables dedicated element clusters for each beam while maintaining compact overall structure, resolving the complexity-efficiency trade-off

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Adaptability or versatility

If multi-carrier operation is implemented with shared elements, then beam coverage is improved, but amplifier efficiency deteriorates due to output back-off and increased power consumption

Engineering Contradiction:
Improvebeam coverage capabilityVSAvoidamplifier power consumption
Core Design Contradiction:
Adaptability or versatilityVSUse of energy by moving object

Solution Approach 1:

The system segments power amplifiers into dedicated groups for each beam, eliminating the need for multi-carrier operation with shared amplifiers. Each beam has its own power amplifiers operating at full efficiency, dramatically reducing total power consumption while maintaining comprehensive beam coverage

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent changes the operational parameters by assigning dedicated power amplifiers to each beam, allowing them to operate at optimal power levels without the output back-off required in shared-element multi-carrier systems. This parameter change directly improves amplifier efficiency and reduces power consumption

Inventive Principle:
Principle #35Parameter changes

3Loss of energy

If dedicated power amplifiers per beam are used, then amplifier efficiency is improved, but device complexity and cost increase

Engineering Contradiction:
Improveamplifier efficiencyVSAvoidamplifier system complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The patent merges the functions of multiple dedicated amplifiers into integrated amplifier clusters associated with each beam. This consolidation reduces the number of discrete components and interconnections, lowering system complexity while maintaining the efficiency benefits of dedicated amplification for each beam

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The amplifier clusters are designed with universal functionality to handle multiple beams through selective activation. Each amplifier cluster can serve its dedicated beam while potentially supporting adjacent beams, reducing the total number of amplifiers needed and simplifying the overall system architecture

Inventive Principle:
Principle #6Universality (Multi-functionality)

4Reliability

If conventional multi-reflector MBA is used with single feed horn per beam, then beam isolation is improved, but system complexity and cost increase due to higher power amplifiers and redundancy requirements

Engineering Contradiction:
Improvebeam isolation performanceVSAvoidantenna system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces the conventional multi-reflector 2D structure with a 3D distributed array of radiating elements throughout a reflective volume. This dimensional transformation achieves superior beam isolation through spatial distribution and phase control, eliminating the need for complex multi-reflector architectures and associated redundancy requirements

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The invention substitutes mechanical/physical separation methods (multiple reflectors) with electromagnetic field control methods (phase and amplitude modulation of distributed elements). This substitution achieves beam isolation through signal processing rather than physical separation, reducing system complexity while improving performance

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

Data Source

PatentEP3270463B1Imaging array fed reflector
Publication Date: 2022.02.16 SPACE SYST LORAL INC
  • EP3270463B1 patent drawingFigure 1A
  • EP3270463B1 patent drawingFigure 1B
  • EP3270463B1 patent drawingFigure 2

AI summary

An imaging array fed reflector for a spacecraft is included in a spacecraft payload subsystem. The payload subsystem includes a multi-beam antenna including a reflector, a plurality of amplifiers, and a plurality of radiating feed elements, the feed elements configured as a phased array, illuminating the reflector, operable at a frequency having a characteristic wavelength (λ), and configured to produce, in a far field at the reflector, a set of contiguous abutting beams. The amplifiers are disposed proximate to the plurality of radiating feed elements. Each radiating feed element has a respective coupling with at least one respective amplifier of the plurality of amplifiers. Each radiating feed element, together with the at least one respective amplifier, is disposed in a closely packed triangular lattice such that separation between adjacent radiating feed elements is not greater than 1.5λ.