Cellular Interferometer Satellite Architecture for Global Earth Observation

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Solution Overview

Problem

Current Earth observation missions rely on large, costly, single-purpose platforms in low Earth orbit, limiting the ability to observe the entire Earth simultaneously and efficiently, with high costs and limited functional versatility.

Innovation Solution

A cellular architecture comprising dozens to hundreds of small, low-cost, free-flying cells in low Earth orbit, each performing primitive sensing tasks that can be combined to execute diverse observing functions, including GNSS radio occultation, Earth gravity field mapping, and global radio holography, using radio frequency and microwave signals for data collection and processing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If large, specialized Earth observing platforms are used, then measurement precision and functional capability are improved, but system cost and device complexity increase significantly

Engineering Contradiction:
Improveobservation capabilityVSAvoidplatform complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent divides a single large Earth observing platform into multiple small, independent cells in low Earth orbit. Each cell performs basic sensing functions, and the collective data from all cells is processed to achieve comprehensive Earth observation. This segmentation reduces individual cell complexity and cost while maintaining overall observation capability through distributed sensing.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent combines the functions of multiple large, specialized observing platforms into a single distributed cellular system. By merging sensing, communication, and data processing capabilities across numerous small cells, the system achieves the functional versatility of multiple platforms without the cumulative cost and complexity of launching separate missions.

Inventive Principle:
Principle #5Merging (Combining)

2Adaptability or versatility

If multiple large observing platforms are deployed to achieve global coverage, then observational versatility is improved, but system cost increases dramatically

Engineering Contradiction:
Improveobservational versatilityVSAvoidsystem cost
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

Each cell in the distributed system is designed with universal sensing capabilities that can observe multiple Earth parameters (ocean, atmosphere, land, ice). The cells use multi-functional instruments that can switch between different observation modes, allowing a single cell to replace multiple specialized platforms and achieving global observational versatility at reduced cost.

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

Solution Approach 2:

The patent uses numerous identical or near-identical cell replicas distributed in low Earth orbit. Each cell is a simplified copy of the basic sensing unit, and the collective array of copies provides comprehensive coverage. This copying approach reduces development and manufacturing costs compared to building multiple unique, specialized platforms.

Inventive Principle:
Principle #26Copying

3Measurement precision

If specialized instruments are carried on each platform, then measurement capability is improved, but device complexity and cost increase

Engineering Contradiction:
Improvesensing capabilityVSAvoidinstrument complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent changes the operational parameters of the sensing system by using many small cells at low Earth orbit altitudes rather than fewer large platforms at higher orbits. This parameter change allows the use of simpler, smaller instruments on each cell while the aggregate data from multiple cells achieves the required measurement precision through statistical combining and interferometric processing.

Inventive Principle:
Principle #35Parameter changes

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 reduces system costs, enables simultaneous global coverage, improves performance through aggregate sensing, and consolidates the functions of multiple platforms into a single, versatile system, allowing for a wide range of observational objectives and future applications.

Implementation Method 1

Cellular interferometer for continuous Earth remote observation

Methodology Applied
Scientific EffectInterference: Interference

Data Source

PatentUS10048382B2Cellular interferometer for continuous Earth remote observation (CICERO) satellite
Publication Date: 2018.08.14 GEOOPTICS INC
  • US10048382B2 patent drawing
  • US10048382B2 patent drawing
  • US10048382B2 patent drawing

AI summary

A fleet of small spacecraft (“cells”) in low Earth orbit combine to form an integrated Earth observing system providing many observations previously requiring distinct sensing systems. Each cell performs a few relatively primitive functions, including emission, reception, sampling, and recording of radio and microwave signals. Each cell observes over a spherical field of view, samples the received signals independently at many small antenna elements, and stores the data from each element. Data from all cells are sent to a common location where they can be combined in diverse ways to realize a wide range of observing functions. These functions may include ionosphere and gravity field mapping; atmospheric radio occultation; ocean, ice, and land altimetry; ocean scatterometry; synthetic aperture radar (SAR) imaging; radar sensing of soil moisture, land cover, and geological surface properties; and interferometric SAR sensing of surface change. The system can also provide real-time messaging, navigation and surveillance functions.