Modular Satellite Imaging for Low-Latency Mission Analytics

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Solution Overview

Problem

The satellite industry faces challenges in designing, integrating, launching, and operating satellites, particularly for researchers lacking expertise. There is a need for a modular satellite testing platform with shorter lead times, using lower-cost and lighter materials, while maintaining performance and allowing for customization. Additionally, there are issues with latency in obtaining analytics data from satellite images and limitations in existing light filtration technologies for orbital devices.

Innovation Solution

A modular satellite system comprising a main body member, controllers, a communication system, a datastore, a power unit, and orbital cameras. This system allows for mission instructions to be executed, data to be stored and transmitted, and includes features like attitude control, light filtering, and image processing. The system is designed to be customizable, use lighter materials, and reduce lead times for development and deployment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional lighter metals like aluminum are used to construct satellite components, then the satellite structure has well understood thermal and electrical properties, but the manufacturing process requires long periods of planning, testing, and lead times

Engineering Contradiction:
Improvethermal and electrical property predictabilityVSAvoidmanufacturing lead time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The satellite is divided into modular components that can be independently manufactured and tested. This segmentation allows parallel development of different modules, reducing overall lead time while maintaining reliability through standardized interfaces and proven subsystems.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Extensive ground testing and validation are performed on satellite components and systems before launch. This preliminary action includes thermal vacuum testing, vibration testing, and electrical characterization to ensure predictable thermal and electrical properties in orbit, reducing the need for lengthy in-orbit testing.

Inventive Principle:
Principle #10Preliminary action

2Quantity of substance

If satellites capture and transmit over 10 million raw photos per day, then comprehensive data is collected, but it takes hours to process and extract analytics from the raw photos

Engineering Contradiction:
Improvedata collection volumeVSAvoidanalytics extraction time
Core Design Contradiction:
Quantity of substanceVSLoss of time

Solution Approach 1:

Analytics extraction and processing are performed in advance on ground-based systems before data is transmitted to end users. This preliminary processing reduces latency by preparing valuable insights ahead of time, so when data is needed, pre-processed analytics are already available rather than requiring hours of processing upon request.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

An intermediary processing system is introduced between data capture and final delivery. This intermediary layer performs initial analytics extraction, filtering, and prioritization on ground-based facilities, reducing the burden on onboard processing and enabling faster delivery of key insights to end users.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Measurement precision

If existing light filtration technologies are used in orbital devices, then basic light filtering is achieved, but the filtration performance is limited and reliability under harsh space conditions is reduced

Engineering Contradiction:
Improvelight filtering capabilityVSAvoidperformance under space conditions
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

Advanced composite light filtering materials are used that combine multiple layers and properties to achieve superior filtration performance. These composite structures provide better wavelength selectivity and maintain reliability under extreme temperature fluctuations and radiation exposure by distributing stress and protecting sensitive filtering layers.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

Protective measures are built into the light filtering system design to withstand harsh space conditions. This includes radiation-hardened materials, thermal protection layers, and redundant filtering elements that are designed beforehand to cushion against the effects of space environment, ensuring continued reliable operation.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

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

The modular satellite system enables efficient data collection and analysis with reduced latency, supports customizable solutions for various missions, and utilizes lighter materials to lower launch costs. It addresses the challenges of expertise gaps, lead time, and material costs in the satellite industry while enhancing performance and reliability.

Implementation Method 1

an orbital camera operable to capture one or more images that may be associated with the mission instruction

Methodology Applied
Scientific EffectPhotoelectric Effect: Photoelectric Effect

Implementation Method 2

a light filter device that may receive one or more wavelengths of light and filter the one or more wavelengths of light received thereby

Methodology Applied
Scientific EffectAbsorption (EM radiation): Absorption (EM radiation)

Data Source

PatentUS20250187757A1System and associated methods for a modular satellite having complex behavior
Publication Date: 2025.06.12 SIDUS SPACE INC
  • US20250187757A1 patent drawing
  • US20250187757A1 patent drawing
  • US20250187757A1 patent drawing

AI summary

A modular satellite system is provided comprising a main body member, one or more controllers, a communication system, a datastore, a power unit, and one or more orbital cameras. The controller(s) may be operable to perform a mission instruction. The communication system may be in communication with the controller(s) and with a client terminal. The datastore may store data accessible by the controller(s). The orbital camera(s) may be operable to capture one or more image(s) associated with the mission instruction, which may be defined as captured image(s). The controller(s) may be operable to detect and identify one or more predetermined object(s) in the one or more captured image(s). The controller(s) may generate a mission analytics packet, and the controller(s) may be operable to transmit the mission analytics packet to the client terminal.