Missile Tracking via Range and Doppler Extraction

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Conventional methods for tracking tactical ballistic missiles suffer from inaccuracy in azimuth and elevation angular data, leading to slow convergence of missile position, velocity, and acceleration estimates, which can result in ineffective defense measures being implemented before the missile reaches its target.

Innovation Solution

A method that collects range and Doppler velocity measurements from multiple radar sensors, time-aligns them, and uses spherical equations to derive exact analytical solutions for position and velocity estimation, focusing on the more accurate range and Doppler data to enhance tracking accuracy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If conventional filtering techniques such as extended Kalman filtering are used with full measurement vectors containing range, angular and Doppler information, then the method can process all available sensor data, but the accuracy of target state estimates converges very slowly due to the inaccuracy of azimuth and elevation angular data

Engineering Contradiction:
Improvetarget state estimation accuracyVSAvoidconvergence time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The invention extracts and uses only the accurate components (range and Doppler measurements) from the full measurement vector, discarding the inaccurate angular measurements. This selective extraction resolves the contradiction by eliminating the source of slow convergence while retaining the useful accurate data for rapid target state estimation.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The invention applies different quality weights to different measurement types, treating range and Doppler measurements as high-quality data while excluding angular measurements. This local quality differentiation allows the system to optimize estimation accuracy by relying on the superior quality measurements without being degraded by the poor quality angular data.

Inventive Principle:
Principle #3Local quality

2Area of stationary object

If the distance between the sensor and the missile increases, then the coverage area of the radar network increases, but the accuracy of the angular data deteriorates rapidly

Engineering Contradiction:
Improveradar network coverage areaVSAvoidangular data accuracy
Core Design Contradiction:
Area of stationary objectVSMeasurement precision

Solution Approach 1:

The invention extracts and utilizes only the range and Doppler measurements from the sensor data, which maintain their accuracy regardless of distance. By excluding the angular measurements that deteriorate with distance, the system achieves rapid convergence of target state estimates even when sensors are positioned far from the missile to maximize coverage area.

Inventive Principle:
Principle #2Taking out (Extraction)

3Reliability

If conventional methods are used to track the missile, then the system can provide tracking information, but the accuracy of position, velocity and acceleration estimates is insufficient for effective defense intervention

Engineering Contradiction:
Improvedefense intervention effectivenessVSAvoidmissile position velocity and acceleration accuracy
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The invention extracts and uses only the accurate range and Doppler measurements to compute target state estimates, eliminating the degrading effect of inaccurate angular measurements. This extraction approach delivers the high position, velocity and acceleration accuracy required for reliable defense intervention effectiveness.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The invention changes the measurement parameters used for estimation from the conventional full measurement vector (including inaccurate angular data) to a selective subset (only range and Doppler). This parameter change transforms the estimation accuracy and enables reliable defense intervention.

Inventive Principle:
Principle #35Parameter 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

This approach rapidly converges to accurate position and velocity estimates, enabling timely defense measures and determining the missile's launching site, with robustness against radar system errors, thus improving the effectiveness of missile defense systems.

Implementation Method 1

Conventional methods of tracking TBMs employ a network of distributed radar sensors to detect and track TBMs. The radar sensors provide positional information in terms of range (distance from the object to the sensor), and angular data (azimuth and elevation), and Doppler velocity information on detected TBMs.

Methodology Applied
Scientific EffectRadar: Radar

Implementation Method 2

The radar sensors provide positional information in terms of range (distance from the object to the sensor), and angular data (azimuth and elevation), and Doppler velocity information on detected TBMs.

Methodology Applied
Scientific EffectDoppler effect: Doppler Effect

Data Source

PatentUS7924213B2Method of and device for tracking an object
Publication Date: 2011.04.12 THALES NEDERLAND BV
  • US7924213B2 patent drawing
  • US7924213B2 patent drawing
  • US7924213B2 patent drawing

AI summary

A method of tracking an object including the steps of: collecting N measurements of range Ri and Doppler velocity Di associated with the object from a plurality M of radar sensors Si each measurement being assigned a time stamp ti; time aligning each Range Ri measurement to a common time stamp tN to provide a corresponding time aligned range Pi for each of the N measurements; using each time aligned Range measurement Pi to define a corresponding spherical equation such that N spherical equations are defined; and deriving analytical solutions from three of the N spherical equations to determine the position vector of the object.