Incremental Neural Network Inference for Spacecraft Navigation

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Solution Overview

Problem

Current space navigation systems rely on ground-based control methods, which are inefficient due to time lags in communication, leading to outdated navigation data and increased uncertainty in spacecraft state.

Innovation Solution

An incremental neural network model inference method is implemented onboard the spacecraft, allowing for real-time updates of navigation state estimates using a neural network model with reduced memory requirements, enabling immediate course corrections.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of time

If ground-based control methods are used for space navigation, then system complexity is reduced, but navigation update time increases and accuracy decreases

Engineering Contradiction:
Improvenavigation update timeVSAvoidonboard computing complexity
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

The patent segments the navigation computation process into discrete incremental steps that can be executed sequentially on onboard hardware. Instead of requiring complete recalculations, the system processes navigation updates in manageable segments that reduce computational burden while maintaining real-time performance.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent implements preliminary action by pre-computing and storing navigation parameters and algorithms on the onboard computer before missions begin. This allows the spacecraft to perform rapid incremental updates during flight without requiring complex real-time calculations, effectively preparing the system in advance for efficient operation.

Inventive Principle:
Principle #10Preliminary action

2Speed

If complete neural network models are loaded into memory, then computation speed improves, but memory requirements increase

Engineering Contradiction:
Improvecomputation speedVSAvoidmemory capacity
Core Design Contradiction:
SpeedVSQuantity of substance

Solution Approach 1:

The patent divides the neural network model into segmentable components that can be loaded and processed in parts rather than requiring the entire model to reside in memory simultaneously. This segmentation allows efficient computation with reduced memory footprint by processing different layers or subsets of the network sequentially.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent implements partial action by loading only the necessary portions of the neural network model into memory at any given time rather than the complete model. This approach maintains adequate computation speed for navigation tasks while significantly reducing the total memory capacity required on the spacecraft.

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS20250130048A1Incremental Neural Network Model Inference
Publication Date: 2025.04.24 ADVANCED SPACE LLC
  • US20250130048A1 patent drawing
  • US20250130048A1 patent drawing
  • US20250130048A1 patent drawing

AI summary

An incremental neural network model inference method for updating a navigation state estimate of a spacecraft includes: reading parameters and functions from a current layer of a neural network model into a memory of a spacecraft computer, performing a transformation on a navigation state estimate with the parameters and functions, saving a transformed navigation state estimate to the memory, and determining whether the current layer of the neural network model is the last layer. When the current layer is not the last layer, the method includes: removing the parameters and functions from the memory; incrementing to a next layer of the neural network model; repeating the steps of reading, transforming, and removing for the next layer of the neural network model until all layers are transformed; when the current layer is the last layer, the method includes: outputting a thrust command.