Dual-Polarization D2D Receive Links Using Alternating Satellite Polarization

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Solution Overview

Problem

Dual circular polarization arrays in satellite communications are costly due to the need for double RF chains, while single polarization arrays result in reduced performance for direct-to-device (D2D) communication.

Innovation Solution

A system using a satellite constellation with single polarization receive DRAs and alternating polarization between two spacecraft, where signals are received by opposite circular polarization antennas and recombined to achieve higher gain, reducing the need for multiple RF chains and improving performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If dual circular polarization arrays are used to maximize reception gain for linearly polarized mobile devices, then reception performance is improved, but system cost increases significantly due to the need to double all RF chains

Engineering Contradiction:
Improvereception performanceVSAvoidsystem cost
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent divides the dual polarization function across multiple satellites instead of implementing it on a single satellite. Each satellite carries only single circular polarization antennas (either LHCP or RHCP), but the constellation collectively provides both polarizations through spatial distribution, eliminating the need to double RF chains on each satellite

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent combines signals from multiple satellites with different polarizations at the ground station. The signal processing system merges LHCP and RHCP signals received from different satellites to reconstruct the complete dual polarization signal, achieving dual polarization performance without dual polarization hardware on each satellite

Inventive Principle:
Principle #5Merging (Combining)

2Device complexity

If single circular polarization antennas are used to reduce cost, then system cost decreases, but reception performance is significantly reduced compared to dual polarization

Engineering Contradiction:
Improvesystem costVSAvoidreception performance
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The patent transitions from a single-satellite approach to a multi-satellite constellation approach, adding the spatial dimension to the polarization reception. By distributing satellites with different polarizations across the sky, the system achieves dual polarization capability through spatial diversity rather than through hardware duplication on each satellite

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

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 allows for significant cost savings and improved reception gain by using single polarization DRAs with signal recombination, maximizing performance while minimizing the number of RF chains and satellite components.

Implementation Method 1

transmit the first digital signal via an optical intersatellite link (OISL)

Methodology Applied
Scientific EffectOptical conversion:

Implementation Method 2

receive the RF signal in left handed circular polarization (LHCP) or right hand circular polarization (RHCP)

Methodology Applied
Scientific EffectElectromagnetic radiation reception:

Data Source

PatentUS20260039384A1System and method for direct to device (D2D) dual polarization alternative for receive links
Publication Date: 2026.02.05 MACDONALD DETTWILER & ASSOC INC
  • US20260039384A1 patent drawing
  • US20260039384A1 patent drawing
  • US20260039384A1 patent drawing

AI summary

Provided is a system and method for direct-to-device (D2D) communication. The system includes a user device for transmitting a radio frequency (RF) signal in linear polarization and a satellite constellation including a first satellite, and a second satellite. The first satellite is configured to receive the RF signal in left handed circular polarization (LHCP) or right hand circular polarization (RHCP), convert the received RF signal to a first digital signal, and transmit the first digital signal via an optical intersatellite link (OISL). The second satellite is configured to receive the RF signal in an opposite polarization of the first satellite, convert the received RF signal to a second digital signal, receive the first digital signal via the OISL, and recombine the first digital signal and the second digital signal.