Sparse Radar Aperture Layout for Immediate Orbit Determination

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Solution Overview

Problem

Current ground RF radar systems are limited in range and size detection, and ground-based optical systems are hindered by lighting conditions and weather, making them inadequate for 24/7 surveillance and threat mitigation in space, particularly in synchronous orbits like geosynchronous orbits, where traditional phased arrays provide poor cross-range resolution and require long-arc tracking.

Innovation Solution

A widely-spaced antenna radar system with aperiodic lattice and unequal element patterns, capable of high angular resolution, operating at high frequencies, and enabling immediate orbit determination without long-arc tracking, using angle of arrival for 3D positioning and cross-range velocity measurement, and mitigating grating lobes, allowing for detection and characterization of smaller objects in synchronous orbits.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional phased array radar systems are used for space surveillance, then they can detect objects in space, but they provide poor cross-range resolution and require long-arc tracking

Engineering Contradiction:
Improvecross-range resolutionVSAvoidtracking time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The patent transitions from traditional 2D planar arrays to 3D volumetric aperture configurations, utilizing elevation angle measurements in addition to azimuth. This dimensional expansion enables immediate 3D positioning and cross-range velocity measurement without requiring long tracking arcs, directly resolving the contradiction between measurement precision and time loss.

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

Solution Approach 2:

The patent divides the radar aperture into multiple widely-spaced sensor elements distributed in three-dimensional space. This segmentation creates a sparse aperture configuration where each element contributes to angular resolution in both azimuth and elevation, enabling high cross-range resolution without requiring a physically large continuous array or extended tracking time.

Inventive Principle:
Principle #1Segmentation

2Reliability

If ground-based optical monitoring systems are used, then they can provide surveillance, but they are limited by lighting conditions, cloud cover and local weather

Engineering Contradiction:
Improvesurveillance availabilityVSAvoidweather interference
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent replaces optical monitoring systems with radio frequency radar systems. This substitution eliminates dependence on visible light and atmospheric transparency, allowing 24/7 surveillance regardless of lighting conditions, cloud cover, or weather. The RF waves penetrate atmospheric conditions that block optical signals, directly resolving the reliability versus weather interference contradiction.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Measurement precision

If widely-spaced antenna arrays are used, then angular resolution improves, but grating lobes are generated

Engineering Contradiction:
Improveangular resolutionVSAvoidgrating lobes
Core Design Contradiction:
Measurement precisionVSObject-generated harmful factors

Solution Approach 1:

The patent employs non-uniform, aperiodic spacing patterns for the antenna elements rather than regular periodic grids. This asymmetric configuration disrupts the formation of grating lobes while maintaining the large baseline distances necessary for high angular resolution. The irregular spacing ensures that constructive interference occurs only in the desired directions, eliminating the harmful grating lobe effect.

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The patent applies different spacing characteristics to different regions of the aperture configuration. By optimizing local element positions and spacing variations throughout the array, the system achieves high overall angular resolution while locally controlling grating lobe formation. Each region's spacing is tailored to contribute to resolution without generating harmful interference patterns.

Inventive Principle:
Principle #3Local quality

4Length of stationary object

If traditional radar systems are used, then they can detect objects, but they are limited in range and size detection capability

Engineering Contradiction:
Improvedetection rangeVSAvoidobject size characterization
Core Design Contradiction:
Length of stationary objectVSMeasurement precision

Solution Approach 1:

The patent utilizes three-dimensional aperture synthesis with elevation component addition, enabling simultaneous measurement of range, cross-range position, and cross-range velocity. This dimensional enhancement provides sufficient geometric diversity to characterize object size and shape at extended ranges, resolving the contradiction between detection range and size characterization precision.

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

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 system achieves very high angular resolution, enabling detection of baseball-sized objects in geosynchronous orbits, immediate orbit determination, and effective threat mitigation, with comprehensive coverage and increased EIRP, allowing for precise imaging and characterization of objects in synchronous orbits without the need for external assets or satellites.

Implementation Method 1

System and method for space domain awareness using a sparse widely-spaced radar aperture

Methodology Applied
Scientific EffectRadar: Radar

Implementation Method 2

receive a signal reflected from the space object

Methodology Applied
Scientific EffectElectromagnetic radiation reflection: Reflection

Implementation Method 3

using angle of arrival for 3D positioning and cross-range velocity measurement

Methodology Applied
Scientific EffectAngle of arrival measurement:

Data Source

PatentUS12184396B2System and method for space domain awareness using a sparse widely-spaced radar aperture
Publication Date: 2024.12.31 SPECIALIZED ARRAYS
  • US12184396B2 patent drawing
  • US12184396B2 patent drawing
  • US12184396B2 patent drawing

AI summary

The present technology describes a widely-spaced antenna radar array for Space Domain Awareness capable of object detection, characterization, imaging and, if unfriendly, threat mitigation. It features (1) very high angular resolution due to the very wide spacing of the sensors, enabling the detection of baseball size objects in GSO, (2) operation at high frequencies enabling characterization of smaller objects because of the ability to mitigate tropospheric effects, (3) operation at varied frequencies enabling threat mitigation and imaging, (4) immediate orbit determination in a single pass without the need for long-arc tracking due to the wide spacing and high precision angle of arrival (AOA) and (5) mitigation of grating lobes caused by the sparse antenna configuration, enabling the sensors to be placed at great distances.