Satellite Constellation Altitude Layering for Collision Avoidance

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Solution Overview

Problem

Satellite constellations with multiple orbital planes at the same altitude face an increased risk of collisions as the number of satellites and planes increases.

Innovation Solution

A satellite constellation forming system that arranges orbital planes with mutually different altitudes to prevent collisions by ensuring satellites in the same orbital plane fly at the same altitude and those in different planes avoid intersections.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If multiple orbital planes are arranged at the same orbital altitude to form a satellite constellation, then the coverage area and number of satellites are increased, but the collision risk between satellites increases

Engineering Contradiction:
Improvecoverage areaVSAvoidcollision risk
Core Design Contradiction:
Area of stationary objectVSReliability

Solution Approach 1:

The patent transitions from a two-dimensional arrangement (multiple orbital planes at the same altitude) to a three-dimensional arrangement (orbital planes at different altitudes). By introducing the altitude dimension as a variable parameter, satellites are distributed in three-dimensional space rather than confined to a single altitude layer, thereby maintaining coverage while reducing collision probability through spatial separation.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The patent changes the orbital altitude parameter from a fixed value (same altitude for all planes) to a variable parameter (different altitudes for different planes). This parameter change allows the system to maintain the benefits of multiple orbital planes while introducing vertical separation to mitigate collision risks, effectively resolving the contradiction between coverage expansion and safety.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If the number of orbital planes and satellites per plane is increased to enhance constellation capability, then the system performance is improved, but the collision risk increases proportionally

Engineering Contradiction:
Improvesystem capabilityVSAvoidcollision risk
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The patent utilizes the altitude dimension to distribute satellites that would otherwise be concentrated in the same orbital plane. By assigning different altitudes to different orbital planes, the system can accommodate a larger number of satellites without increasing the density in any single plane, thereby enhancing overall capability while maintaining safety through three-dimensional dispersion.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The patent segments the satellite constellation into multiple altitude layers, with each orbital plane occupying a distinct altitude level. This segmentation strategy divides the potentially congested single-layer configuration into multiple separated layers, allowing each layer to operate independently with reduced collision probability while the aggregate system achieves enhanced capability.

Inventive Principle:
Principle #1Segmentation

3Area of stationary object

If satellites are arranged in multiple orbital planes at the same altitude, then the constellation provides comprehensive coverage, but collision avoidance becomes more difficult

Engineering Contradiction:
Improvecoverage areaVSAvoidcollision avoidance complexity
Core Design Contradiction:
Area of stationary objectVSDevice complexity

Solution Approach 1:

The patent introduces altitude as an additional dimension for collision avoidance, transforming the problem from two-dimensional (within the same orbital plane) to three-dimensional (across multiple altitude levels). This dimensional expansion provides natural vertical separation between orbital planes, significantly simplifying collision avoidance strategies while preserving comprehensive ground coverage through the multi-plane configuration.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Data Source

PatentUS12595077B2Space traffic management system, space traffic management device, ground facility and operation method for avoiding collision during orbital descent
Publication Date: 2026.04.07 MITSUBISHI ELECTRIC CORP
  • US12595077B2 patent drawing
  • US12595077B2 patent drawing
  • US12595077B2 patent drawing

AI summary

A satellite constellation forming system (100) forms a satellite constellation (20). The satellite constellation (20) is composed of a satellite group (300). In the satellite constellation (20), the satellite group (300) provides a service cooperatively. The satellite constellation (20) has a plurality of orbital planes in which a plurality of satellites (30) fly at the same orbital altitude in each orbital plane (21). A satellite constellation forming unit (110) forms the satellite constellation (20) in which orbital altitudes of the plurality of orbital planes (21) are mutually different.