HAPS Relay Segments Satellite Feeder Link for MIMO RF and FSO

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Solution Overview

Problem

Conventional ground-to-satellite free-space-optical (FSO) links are hindered by atmospheric impairments such as attenuation, scintillation, beam wandering, and pointing errors, as well as the requirement for an unobstructed line-of-sight, which is often obstructed by clouds, leading to frequent link failures and high deployment costs.

Innovation Solution

A relay-assisted hybrid radio frequency/free-space-optical (RF/FSO) ground-satellite link is implemented using a high-altitude platform station (HAPS) that splits the link into a ground-to-HAPS MIMO RF link and a HAPS-to-satellite FSO link, mitigating atmospheric impairments and reducing bandwidth and propagation disparities between RF and FSO links.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a ground-to-satellite FSO link is implemented, then data rate is improved, but reliability deteriorates due to atmospheric impairments and cloud obstruction

Engineering Contradiction:
Improvedata rateVSAvoidlink reliability
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The ground-to-satellite link is segmented into two separate links: a ground-to-HAPS RF link and a HAPS-to-satellite FSO link. This segmentation allows the FSO link to operate from elevated altitude where atmospheric impairments are reduced, while the RF link handles the ground segment, thereby maintaining high data rates while improving overall link reliability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A high-altitude platform station (HAPS) is introduced as an intermediary node between the ground and satellite. The HAPS serves as a relay that receives signals via RF from the ground and transmits via FSO to the satellite, mitigating the effects of atmospheric turbulence and cloud obstruction by operating the FSO link from elevated altitude.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If multiple redundant optical gateways are deployed to overcome cloud attenuation, then reliability is improved, but deployment cost increases

Engineering Contradiction:
Improvelink availabilityVSAvoiddeployment cost
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Instead of adding redundancy in the horizontal dimension (multiple ground-based gateways spread over large geographical regions), the solution moves to the vertical dimension by deploying a single HAPS at high altitude (approximately 18-24 kilometers). This dimensional shift allows a single platform to access clearer atmospheric conditions above most cloud layers, achieving reliability improvement without proportional cost increase.

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

3Reliability

If an RF link is used as backup when optical link has outage, then reliability is improved, but bandwidth is reduced

Engineering Contradiction:
Improvelink availabilityVSAvoidfeeder-link capacity
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system dynamically switches between RF and FSO links based on atmospheric conditions and operational requirements. The HAPS can communicate with the ground via RF when needed and with the satellite via FSO when optimal, allowing the system to adapt to changing conditions while maintaining high capacity through the FSO link during normal operation.

Inventive Principle:
Principle #15Dynamics

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 significantly improves the reliability of the ground-to-satellite link by reducing the effects of atmospheric impairments and bandwidth disparities, while also lowering the costs associated with deployment and maintenance.

Implementation Method 1

a first sub-link from a ground terminal to the HAPS relay station implemented as a line-of-sight (LoS) multiple-in-multiple-out (MIMO) radio frequency (RF) link, and a second sub-link from the HAPS relay station to a satellite implemented as a free-space-optical (FSO) link

Methodology Applied
Scientific EffectElectromagnetic radiation: Electromagnetic Induction

Data Source

PatentUS20250158711A1Relay-assisted high-capacity satellite feeder links with integrated line-of-sight MIMO RF and optical channels via haps
Publication Date: 2025.05.15 HUGHES NETWORK SYST
  • US20250158711A1 patent drawing
  • US20250158711A1 patent drawing
  • US20250158711A1 patent drawing

AI summary

Techniques are described for providing satellite communications via a relay-assisted hybrid radio frequency/free-space-optical (RF/FSO) ground-satellite link. A high-altitude platform station (HAPS) splits the ground-to-satellite link into a ground-to-HAPS line-of-sight (LoS) multiple-in-multiple-out (MIMO) radio frequency (RF) link, and a HAPS-to-satellite FSO link. The approach mitigates the effects of atmospheric impairments on the FSO link, while also appreciably reducing adverse effects of bandwidth and propagation disparity between the RF and FSO links.