Autonomous Flight Safety System for Aerial Vehicles

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Solution Overview

Problem

Current flight termination systems rely on human intervention to monitor and decide on flight path deviations, which can be slow and inefficient, particularly in critical situations where rapid decision-making is necessary to ensure safety and prevent hazards.

Innovation Solution

An autonomous flight safety system onboard the aerial vehicle, utilizing multiple sensors and processors to independently analyze flight data and generate flight termination signals, allowing for real-time autonomous decision-making and termination of the flight if safety boundaries are violated.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If human intervention is used to monitor and decide on flight path deviations, then decision-making can be made with human judgment, but the response time is slow and inefficient

Engineering Contradiction:
Improveflight termination decision reliabilityVSAvoidresponse time for flight termination
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The flight safety assembly performs autonomous flight termination decisions without human intervention. The processor automatically analyzes flight data from multiple sensors, determines instantaneous impact points, and generates termination signals when safety boundaries are violated, enabling the system to serve itself in critical decision-making

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces the mechanical human decision-making process with an automated electronic system. The processor substitutes human judgment with algorithm-based analysis of sensor data, eliminating the time delay associated with human reaction while maintaining reliable termination decisions through programmed safety criteria

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

2Reliability

If multiple sensors and independent analysis paths are used, then measurement reliability is improved, but device complexity increases

Engineering Contradiction:
Improveflight termination decision reliabilityVSAvoidsensor and processor complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system divides the flight safety function into multiple independent analysis paths, each processing data from specific sensors separately. This segmentation allows parallel processing of different sensor inputs (accelerometer, GPS, barometer) through distinct computational routes, improving reliability through diversity while organizing complexity into manageable modular segments

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system implements three independent analysis paths when two might suffice for redundancy. This excessive action provides enhanced reliability by ensuring that even if one or two paths fail, the third can still make a safe termination decision, prioritizing safety over minimal complexity

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS9429403B2Methods and apparatuses for autonomous flight termination
Publication Date: 2016.08.30 NORTHROP GRUMMAN SYSTEMS CORP
  • US9429403B2 patent drawing
  • US9429403B2 patent drawing
  • US9429403B2 patent drawing

AI summary

A flight safety assembly onboard an aerial vehicle includes a first sensor configured to sense first information related to flight of the aerial vehicle and a second sensor configured to sense second information related to the flight of the aerial vehicle. A sensor input is adapted to receive third information related to the flight of the aerial vehicle. A processor is operably coupled to the first sensor, the second sensor, and the sensor input. The processor is configured to determine three independent instantaneous impact points for the aerial vehicle by independently analyzing each of the first information, the second information and the third information. The processor is also configured to generate three independent onboard flight termination indicators for each of the three independent instantaneous impact points that intersects with a region to be protected.