Helicopter Obstacle Detection Radar System

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Solution Overview

Problem

Current aerial navigation aids, such as TAWS and HELLAS systems, fail to effectively protect helicopters from collisions with obstacles, particularly during takeoff and landing phases, as they do not account for lateral or rear obstacles and are not designed to detect mobile obstacles, leading to inadequate warning times for critical situations.

Innovation Solution

A monitoring device that uses real-time detection of obstacles and terrain via short-range radar technology, calculates criticality parameters, and generates audible and visual alerts to inform pilots of potential collisions, providing a comprehensive view of the aircraft's environment and enabling timely reactions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If TAWS systems are used for terrain anticollision monitoring, then terrain collision protection is improved, but lateral and rear obstacle detection is not provided

Engineering Contradiction:
Improveterrain collision protectionVSAvoidobstacle detection coverage
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The monitoring system is divided into multiple independent detection units positioned at different locations on the aircraft (front, rear, lateral sides), each responsible for monitoring specific zones. This segmentation allows comprehensive coverage of all directions while maintaining specialized detection capabilities for each zone.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The monitoring device integrates multiple detection functions into a single system that can detect terrain, fixed obstacles, and mobile obstacles simultaneously. The system processes various types of obstacles using unified detection and evaluation algorithms, providing versatile protection across different obstacle types and locations.

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

2Measurement precision

If HELLAS systems are used for obstacle detection, then fixed obstacle detection is improved, but mobile obstacle detection is not provided

Engineering Contradiction:
Improvefixed obstacle detectionVSAvoidmobile obstacle detection
Core Design Contradiction:
Measurement precisionVSAdaptability or versatility

Solution Approach 1:

The system dynamically adapts its detection and evaluation parameters based on the movement characteristics of obstacles. For mobile obstacles, the system adjusts detection sensitivity and criticality evaluation in real-time based on relative velocity and trajectory predictions, enabling effective detection of moving targets while maintaining precision for fixed obstacles.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The monitoring device changes detection and evaluation parameters according to obstacle type and motion state. Detection thresholds, criticality weights, and alert timing are adjusted based on whether obstacles are stationary or moving, allowing optimized performance across different obstacle categories.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If TAWS alert functions are used, then collision warning is provided, but warning time is insufficient for critical situations

Engineering Contradiction:
Improvecollision warningVSAvoidwarning time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system performs preliminary detection and evaluation of potential collision risks before they become critical threats. By continuously monitoring obstacle proximity, relative velocity, and trajectory, the system identifies developing risks early and provides progressive warnings that give pilots adequate time to react before collision becomes imminent.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The monitoring device provides continuous feedback to the pilot about obstacle proximity and collision risk levels. The system updates warning intensity and frequency based on changing situational parameters, maintaining appropriate alert levels that guide pilot response while providing sufficient time for corrective action.

Inventive Principle:
Principle #23Feedback

4Adaptability or versatility

If comprehensive obstacle detection is implemented, then detection coverage is improved, but device complexity increases

Engineering Contradiction:
Improvedetection coverageVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

Multiple detection functions and processing algorithms are merged into a single integrated monitoring device. The system combines terrain monitoring, fixed obstacle detection, and mobile obstacle tracking in one unified platform, reducing overall system complexity while maintaining comprehensive detection coverage through shared hardware and software resources.

Inventive Principle:
Principle #5Merging (Combining)

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 significantly enhances flight safety by reducing crew stress and improving decision-making through accurate, real-time information on obstacles and their movement relative to the aircraft, thereby preventing collisions with both fixed and mobile artificial obstacles.

Implementation Method 1

A monitoring device that uses real-time detection of obstacles and terrain via short-range radar technology

Methodology Applied
Scientific EffectRadar: Radar

Data Source

PatentUS20120215436A1Device and method for monitoring the obstructions in the close environment of an aircraft
Publication Date: 2012.08.23 THALES SA
  • US20120215436A1 patent drawing
  • US20120215436A1 patent drawing
  • US20120215436A1 patent drawing

AI summary

The invention relates to a device for monitoring obstructions for an aircraft including data storage, an anticollision device and viewing devices, wherein the monitoring device comprises a detector to detect in real-time obstructions, of terrain type and of human constructions type, in a close environment of the aircraft in a flight situation, a sensor to identify the obstructions at risk calculating identification parameters, a circuit to calculate criticality of the obstructions, a display to display both the obstructions with the identification and criticality parameters of the obstructions, and a generator of alerts to describe the situation according to a combination of the identification and criticality parameters. One or more embodiments of the invention is a monitoring system adapted for zones close to the aircraft and in the flight zones not visible to the crew. One or more embodiments of the invention applies particularly to helicopters executing low-altitude flights. It relates more particularly to military carriers such as rescue carriers.