Cable-Assisted UAV PTOL for Moving Vehicle Recovery

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing systems fail to provide safe and efficient point take-off and landing (PTOL) capabilities for large-wingspan fixed-wing UAVs on moving vehicles, particularly in challenging conditions such as strong winds, turbulence, and obstacles, due to the UAV's inability to hover and the interference of wings with ship deck elements.

Innovation Solution

A PTOL system with launch and recovery arm assemblies, including a main pole, receiving latch, and cable release/retraction mechanism, which guides UAVs to latch onto a receiving latch, allowing for controlled landing and take-off on moving vehicles, even in adverse weather conditions, using suspension cables and latching elements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single arresting line is used to stop the UAV, then the landing system is simple, but the UAV may be left hanging and damaged

Engineering Contradiction:
Improvelanding system structureVSAvoidUAV safety during landing
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The arresting line system is divided into multiple segments: a first arresting line for initial deceleration and a second arresting line for final stopping and securing. This segmentation allows the UAV to be stopped in a controlled manner and prevents it from being left hanging, resolving the contradiction between system simplicity and landing safety.

Inventive Principle:
Principle #1Segmentation

2Adaptability or versatility

If the UAV lands on a moving vehicle without a runway, then PTOL capability is achieved, but the large wingspan interferes with deck elements

Engineering Contradiction:
ImprovePTOL capabilityVSAvoidwing interference with deck elements
Core Design Contradiction:
Adaptability or versatilityVSObject-affected harmful factors

Solution Approach 1:

The landing system uses vertical arresting lines extending upward from the vehicle deck to intercept the UAV in the air space above the deck. This dimensional approach allows the UAV to be captured and stopped before its wings can interfere with deck elements, enabling PTOL capability while avoiding wing interference.

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

3Productivity

If the UAV is abruptly stopped in flight, then landing is achieved quickly, but damage to the UAV may occur

Engineering Contradiction:
Improvelanding speedVSAvoidUAV integrity
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system employs multiple arresting lines that engage sequentially to progressively decelerate the UAV. The first arresting line provides initial deceleration, and the second arresting line provides final stopping with proper tensioning, preventing abrupt stops that could damage the UAV while maintaining quick landing capability.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Data Source

PatentEP3680181B1Cable-assisted point take-off and landing of unmanned flying objects
Publication Date: 2025.12.03 YOFFE MEIR
  • EP3680181B1 patent drawingFigure 1A~1C
  • EP3680181B1 patent drawingFigure 2
  • EP3680181B1 patent drawingFigure 3

AI summary

The present invention provides systems and methods for point take-off and landing (PTOL) of unmanned flying objects onto a confined landing surface associated with a landing body.