Satellite RF Interference Avoidance Using Visibility Windows

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Solution Overview

Problem

Conventional spacecraft systems lack the ability to autonomously plan and react to real-time Radio Frequency (RF) and Electromagnetic Interference (EMI) events, relying on pre-planned responses based on past detection and classification, and do not perform autonomous avoidance planning.

Innovation Solution

A method and circuit for predicting and avoiding RF interference by obtaining orbit and transmission data, calculating visibility windows, comparing transmission parameters and orientations, generating a course of action, and autonomously executing it to avoid interference, using a spacecraft's processing circuit.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If conventional pre-planned RFI response methods are used, then system complexity is reduced and ease of operation is improved, but the spacecraft cannot react to real-time RFI events and reliability deteriorates

Engineering Contradiction:
Improveease of operationVSAvoidreliability
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The system performs preliminary RFI prediction by calculating visibility windows and potential interference scenarios in advance, but executes the actual avoidance response autonomously in real-time based on predicted events, combining pre-planning with real-time adaptation

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The spacecraft performs autonomous RFI avoidance planning and execution without requiring continuous human intervention, with the system self-managing the detection, analysis, and response execution while operators only review and approve final actions

Inventive Principle:
Principle #25Self-service

2Reliability

If autonomous real-time RFI prediction and avoidance planning is implemented, then reliability and productivity are improved, but device complexity increases

Engineering Contradiction:
ImprovereliabilityVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The autonomous RFI avoidance system is divided into distinct functional modules: RFI prediction module (calculating visibility windows and potential interference), analysis module (comparing transmission parameters and orientations), course of action generation module (developing avoidance strategies), and execution module (implementing selected actions), allowing complex functionality to be managed through modular components

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system uses a unified processing framework that handles multiple RFI scenarios (different types of interference, various orbital configurations, multiple spacecraft) through the same algorithms and decision-making processes, reducing overall system complexity despite increased capabilities

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

3Loss of time

If autonomous avoidance planning is implemented, then decision-making speed is improved and loss of time is reduced, but ease of operation deteriorates due to increased automation complexity

Engineering Contradiction:
Improveloss of timeVSAvoidease of operation
Core Design Contradiction:
Loss of timeVSEase of operation

Solution Approach 1:

The system implements feedback loops where predicted RFI events and selected avoidance actions are communicated to operators for review and approval, allowing autonomous operation to proceed while maintaining operator oversight and simplifying the user interface to show only critical decisions requiring human input

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS12562809B2Prediction and avoidance of radio frequency interference
Publication Date: 2026.02.24 RAYTHEON CO
  • US12562809B2 patent drawing
  • US12562809B2 patent drawing
  • US12562809B2 patent drawing

AI summary

System and method for prediction and avoidance of RF interference for a satellite from one or more of resident space objects (RSOs) includes: obtaining orbit data and transmission data for the satellite and the plurality of RSOs; calculating a visibility window; performing comparison of transmission parameters; calculating an orientation of each of the RSOs; when there is a match of transmission parameters and the orientation is within a predetermined threshold, adding the compatible RSO to a compatible RSO list; generating a course of action (COA); scoring each of the compatible RSO; selecting a best scored COA; scheduling the first course of action; and autonomously executing the first course of action by the satellite to avoid RFI.