Flying Object Coping System with Dynamic Communication Route Search

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Solution Overview

Problem

Surveillance from low Earth orbit (LEO) satellites faces challenges due to the need for numerous satellites and dynamic satellite positions, making continuous detection and communication of flying objects difficult and requiring complex configurations and data transmission systems.

Innovation Solution

A flying object coping system comprising multiple surveillance and communication satellites with ground centers that transmit directive commands, utilizing a communication route search device to establish efficient data pathways for quasi-real-time information transmission of flying object data to coping assets on land, sea, and air.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If surveillance is conducted from low Earth orbit satellites, then detection performance is improved due to smaller distance to flying objects, but the number of satellites required increases enormously and system complexity increases

Engineering Contradiction:
Improvedetection performanceVSAvoidnumber of satellites
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent combines surveillance satellites and communication satellites into a unified satellite system where communication satellites serve dual purposes: maintaining communication circuits and transmitting surveillance data. This merging reduces the total number of satellites needed while preserving detection performance through the use of multiple LEO satellites for surveillance and the same constellation for data transmission.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

Communication satellites are designed to perform multiple functions: maintaining communication circuits with ground stations and transmitting surveillance data from surveillance satellites. This multi-functionality eliminates the need for separate dedicated communication infrastructure, reducing system complexity while enabling continuous surveillance operations.

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

2Measurement precision

If low Earth orbit satellites are used for surveillance, then detection capability is enhanced, but continuous surveillance and communication require dynamic reconfiguration of satellite positions and communication routes

Engineering Contradiction:
Improvedetection capabilityVSAvoidcontinuous surveillance operation
Core Design Contradiction:
Measurement precisionVSEase of operation

Solution Approach 1:

The system dynamically adjusts communication routes and satellite positions to maintain continuous surveillance capability. As LEO satellites move along their orbits, the communication ground center continuously reconfigures communication circuits to track satellite positions, enabling uninterrupted data transmission and surveillance coverage despite the dynamic nature of LEO operations.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The communication ground center receives real-time information about satellite positions and communication circuit status, using this feedback to dynamically reconfigure communication routes. This feedback mechanism ensures continuous surveillance operation by automatically adapting to satellite motion and maintaining optimal communication pathways.

Inventive Principle:
Principle #23Feedback

3Reliability

If numerous LEO satellites are deployed for continuous surveillance, then coverage is improved, but data transmission complexity and required communication infrastructure increase enormously

Engineering Contradiction:
Improvecontinuous surveillance coverageVSAvoidcommunication infrastructure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent merges communication and surveillance functions into a single integrated system. Communication satellites that would traditionally be separate entities are instead utilized as part of the surveillance constellation, transmitting surveillance data through the same satellite network that provides communication services. This integration dramatically reduces communication infrastructure requirements while maintaining continuous coverage.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The satellite system is designed with universal functionality where communication satellites serve both as communication relays and as data transmission channels for surveillance information. This multi-functionality eliminates the need for separate dedicated communication infrastructure, reducing overall system complexity while enabling reliable continuous surveillance.

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

4Ease of operation

If stationary orbit satellites are used, then communication circuits appear locked relative to earth fixed coordinates simplifying configuration, but distance to flying objects increases reducing infrared detection performance

Engineering Contradiction:
Improvecommunication circuit configurationVSAvoidinfrared detection performance
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The system transitions from static GEO satellite configuration to dynamic LEO satellite operations, where satellites continuously move along their orbits. This dynamic approach provides closer proximity to flying objects for improved infrared detection, while the ground control centers dynamically adjust communication circuits to track satellite positions, maintaining operational effectiveness despite the loss of geometric locking.

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

Enables quasi-real-time transmission of flying object information to coping systems, improving detection and response capabilities by optimizing communication routes and satellite configurations.

Implementation Method 1

detect a temperature rise caused by atmospheric friction when the flying object enters the atmosphere with infrared

Methodology Applied
Scientific EffectInfrared radiation: Infrared Radiation

Data Source

PatentUS20240109674A1Flying object coping system, surveillance ground center, coping ground center, communication route search device, flight path prediction device, and coping asset selection device
Publication Date: 2024.04.04 MITSUBISHI ELECTRIC CORP
  • US20240109674A1 patent drawing
  • US20240109674A1 patent drawing
  • US20240109674A1 patent drawing

AI summary

In a flying object coping system (1000), a surveillance ground center (311) transmits, to a communication ground center (321), an ID, time information, and position information of a surveillance satellite (100) which will transmit flying object information, an ID, time information, and position information of a surveillance satellite (100) which will receive the flying object information, and position information of a coping system (330). The communication ground center (321) is equipped with a communication route search device (470), which searches for a communication route for satellite information. The communication ground center (321) transmits directive commands to the communication satellite group of the communication system (320) based on a search result from the communication route search device (470).