UAS Flight Boundary Limiting Control for Restricted Airspace

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Solution Overview

Problem

Current systems for unmanned aerial systems (UAS) lack reliable means to prevent midair collisions with manned aircraft, as they cannot physically prevent UAS from entering restricted airspace, posing a catastrophic risk.

Innovation Solution

A flight limiting controller (FLC) system that determines the UAS's position relative to flight boundaries and activates limitations such as warnings, autopilot commands, parachute deployment, or propulsion device adjustments to prevent crossing of prohibited areas, ensuring a high system integrity of at least 1*10−7 to prevent collisions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If flight limitation functions are made highly reliable with system integrity of at least 1*10−7 to prevent catastrophic midair collisions, then safety is improved, but the cost and complexity of the UAS system increases

Engineering Contradiction:
Improveflight limitation system integrityVSAvoidsupervisory controller complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The supervisory controller is segmented into distinct functional modules: GPS position acquisition module, boundary data storage module, position comparison module, and flight limitation control module. This segmentation allows each component to be independently designed, tested, and validated for reliability while maintaining overall system integrity of at least 1*10−7 without excessive complexity.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS20250095504A1Supervisory safety system for controlling and limiting unmanned aerial system (UAS) operations
Publication Date: 2025.03.20 AEROVIRONMENT INC
  • US20250095504A1 patent drawing
  • US20250095504A1 patent drawing
  • US20250095504A1 patent drawing

AI summary

Systems, devices, and methods for determining, by a processor, an unmanned aerial system position relative to at least one flight boundary; and effecting, by the processor, at least one flight limitation of a flight limiting device if the determined unmanned aerial system position crosses the at least one flight boundary.