Strip-Shaped Missile Radar Antennas for Tip-Independent Target Tracking

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Solution Overview

Problem

Existing missile guidance systems face challenges in achieving accurate target navigation and detection while simplifying the implementation of radar sensor units.

Innovation Solution

A guided missile equipped with a radar sensor unit featuring strip-shaped radar antennas aligned along the missile's longitudinal axis, allowing for improved target acquisition, detection, and tracking by adapting the field of view alignment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If radar sensor units are integrated into the missile tip, then target acquisition accuracy is improved, but the missile tip functionalization is limited

Engineering Contradiction:
Improvetarget acquisition accuracyVSAvoidmissile tip functionalization
Core Design Contradiction:
Measurement precisionVSAdaptability or versatility

Solution Approach 1:

The radar sensor unit is segmented from the missile tip structure, with the antenna mounted on the missile body surface rather than integrated into the tip. This allows the missile tip to be functionalized independently for other purposes while the radar sensor performs target acquisition on the missile body.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The radar antenna is mounted on the circumferential surface of the missile body, utilizing the lateral dimension rather than the longitudinal tip area. This spatial repositioning resolves the conflict between tip functionalization needs and radar sensor integration.

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

2Measurement precision

If complex radar sensor units are used to improve target detection accuracy, then measurement precision is improved, but device complexity increases

Engineering Contradiction:
Improvetarget detection accuracyVSAvoidradar sensor unit implementation
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The strip-shaped radar antenna serves multiple functions: target acquisition, target detection, and field of view alignment. This multi-functionality reduces the need for separate specialized components, thereby simplifying the overall radar sensor unit implementation while maintaining detection accuracy.

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

Solution Approach 2:

The invention uses a strip-shaped antenna geometry with specific dimensional parameters (length significantly greater than width) to achieve enhanced target detection accuracy through improved radar cross-section and directional characteristics, avoiding the need for more complex sensor architectures.

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

The proposed solution enhances the accuracy and reliability of target acquisition, tracking, and navigation, while allowing for flexible functionalization of the missile tip and easy retrofitting of radar sensor systems.

Implementation Method 1

The radar sensor unit contains at least one radar antenna that is strip-shaped in the longitudinal direction

Methodology Applied
Scientific EffectRadar: Radar

Data Source

PatentUS12203729B2Missile, in particular guided missile, having a radar sensor unit
Publication Date: 2025.01.21 DIEHL DEFENCE GMBH & CO KG
  • US12203729B2 patent drawing
  • US12203729B2 patent drawing
  • US12203729B2 patent drawing

AI summary

A missile, in particular a guided missile, has a missile body and a radar sensor unit for acquiring a target object. The radar sensor unit contains at least one radar antenna, strip-shaped in the longitudinal direction, that is mounted or integrated on a circumferential surface of the missile body such that the longitudinal direction of the at least one strip-shaped radar antenna is aligned in the direction of the missile longitudinal axis.