Doppler Radar Rotor Feature Extraction for Hovering Helicopter Detection

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Solution Overview

Problem

Conventional airborne look-down Doppler radars face challenges in detecting and classifying hovering and slow-moving helicopters due to their body Doppler signals merging with ground clutter, making it difficult to distinguish and track these targets effectively.

Innovation Solution

A system and method that processes radar returns to create a 1-D Doppler profile or 2-D Range-Doppler Map, allowing for the identification and extraction of rotor features such as bandwidth, activity, and shape from the extended rotor return, which are used to classify potential targets as helicopters, even when body Doppler is obscured by clutter.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If conventional look-down Doppler radar is used to detect helicopters, then the radar can detect fast-moving targets with high signal-to-clutter ratio, but hovering or slow-moving helicopters cannot be detected because their body Doppler merges with ground clutter

Engineering Contradiction:
Improvetarget detection capabilityVSAvoidground clutter interference
Core Design Contradiction:
Measurement precisionVSObject-affected harmful factors

Solution Approach 1:

The patent segments the target return signal into two distinct components: body Doppler (from the helicopter fuselage) and rotor Doppler (from the rotating rotor assembly). By separating these components in the Doppler spectrum, the system can identify the rotor return as a distinct feature that extends beyond the clutter region, enabling detection of hovering helicopters whose body Doppler is merged with ground clutter.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent extends the detection approach from one-dimensional body Doppler analysis to two-dimensional analysis by incorporating rotor rotation dynamics. The rotor assembly's rotation creates an extended Doppler return that spans a wider frequency range, providing an additional dimension for target identification that is independent of the helicopter's translational velocity.

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

2Measurement precision

If the seeker estimates range and range-rate from rotor return, then hovering helicopters can be detected, but the measurements are conflicting and scintillating causing the seeker to disregard the rotor return

Engineering Contradiction:
Improverange and range-rate estimationVSAvoidmeasurement consistency
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The patent introduces an intermediary classification process that acts as a mediator between the raw rotor return signal and the tracking system. The classification processor analyzes rotor-specific features (such as the extended Doppler bandwidth and characteristic spectral shape) to verify target identity, then provides reliable range and range-rate estimates to the tracking system. This intermediary layer filters out the scintillating and conflicting measurements, converting them into stable tracking data.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Productivity

If standard detection techniques are used, then fast-moving helicopters can be classified with high confidence, but hovering helicopters are misclassified or undetected due to body Doppler merging with clutter

Engineering Contradiction:
Improvetarget classification accuracyVSAvoidtarget identification difficulty
Core Design Contradiction:
ProductivityVSDifficulty of detecting and measuring

Solution Approach 1:

The patent changes the 'color' or spectral signature that the radar looks for when classifying targets. Instead of relying on the narrow body Doppler signature of conventional targets, the system is trained to recognize the distinctive spectral pattern of rotor returns - specifically, the extended bandwidth and characteristic shape in the Doppler spectrum. This spectral 'color change' enables the classification system to identify hovering helicopters that would otherwise be indistinguishable from ground clutter.

Inventive Principle:
Principle #32Color 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

Enables robust detection and classification of hovering and slow-moving helicopters, providing accurate range, range-rate, and angle estimates for successful tracking and guidance of missiles.

Implementation Method 1

airborne look-down Doppler radar tracking of hovering helicopters using rotor features

Methodology Applied
Scientific EffectDoppler effect: Doppler Effect

Implementation Method 2

transmit an electromagnetic signal 12, typically an X-band radio wave

Methodology Applied
Scientific EffectElectromagnetic radiation: Electromagnetic Induction

Data Source

PatentEP2033011B1Airborne look-down doppler radar tracking of hovering helicopters using rotor features
Publication Date: 2017.02.08 RAYTHEON CO
  • EP2033011B1 patent drawing
  • EP2033011B1 patent drawing
  • EP2033011B1 patent drawing

AI summary

A system and method is presented for detecting and classifying slow-moving and hovering helicopters from a missile's look-down Doppler radar that is compatible with the existing base of Doppler radars. This approach uses definable attributes of a helicopter rotor assembly and its extended Doppler rotor return to differentiate "rotor samples" from other samples (steps 123, 125), extract features such as bandwidth, activity, angle, and shape from the rotor samples (step 127), and classify a potential target as a helicopter or other based on the extracted rotor features and the known attributes of the helicopter rotor assembly (step 129). A target report including a classification target, range, range-rate, and angle of the extended rotor return is suitably passed to a tracking processor (step 121).