Kite-Suspended Tether Recovery for Runway-Free UAV Capture

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Solution Overview

Problem

Current UAV recovery methods lack flexibility and efficiency, particularly in recovering UAVs without the use of runways, and often require complex systems or high costs.

Innovation Solution

A system utilizing a kite to suspend and control a tether line, allowing for the steerable recovery of UAVs from stationary or moving platforms, such as ships, by coordinating the movement of the kite and UAV to ensure controlled deceleration and capture via the tether line.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a kite is used to suspend and control a tether line for UAV recovery, then the flexibility and adaptability of recovery locations are improved, but the device complexity increases due to the need to coordinate kite and UAV movements

Engineering Contradiction:
Improverecovery location flexibilityVSAvoidsystem coordination complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The kite acts as an intermediary element between the recovery platform and the UAV. It suspends the tether line and uses wind forces to control the line's position and tension, mediating the interaction between the platform and the approaching UAV without requiring complex active control systems on the platform itself.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The kite utilizes natural wind forces to maintain tension in the tether line and position itself, rather than requiring powered actuators or complex control systems. The kite's aerodynamic properties enable it to self-adjust and maintain the necessary configuration for UAV capture passively.

Inventive Principle:
Principle #25Self-service

2Ease of manufacture

If the tether line is used to capture the UAV, then the cost is reduced compared to traditional runway systems, but the force management during capture becomes more challenging

Engineering Contradiction:
Improvesystem costVSAvoidcapture force management
Core Design Contradiction:
Ease of manufactureVSForce

Solution Approach 1:

The system is designed to manage the impact forces that occur when the UAV contacts the tether line. The kite's position and the line's tension are controlled beforehand to ensure that the capture force is within acceptable limits, cushioning the impact similar to how a parachute reduces landing force.

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

Solution Approach 2:

The system controls the physical parameters of the tether line (tension, angle, length) and the kite's position to optimize the capture process. By adjusting these parameters, the system manages the force distribution during UAV capture, ensuring safe deceleration without requiring expensive active control systems.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If the kite is steered to facilitate controlled impact, then the reliability of UAV capture is improved, but the ease of operation decreases due to the need for coordinated movement control

Engineering Contradiction:
ImproveUAV capture reliabilityVSAvoidkite and UAV coordination
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system uses feedback from tracking the UAV's position and the kite's response to wind forces to adjust the tether line orientation and kite position. This feedback loop enables reliable capture by continuously adapting the system configuration to match the approaching UAV's trajectory and speed.

Inventive Principle:
Principle #23Feedback

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

Enables effective and cost-efficient UAV recovery in various locations, including unprepared areas and smaller vessels, by maintaining tension in the tether line and directing the kite to facilitate a controlled impact, reducing the force on the UAV and ensuring successful capture.

Implementation Method 1

a kite (e.g., a parafoil kite) that generates lift to support a tether line

Methodology Applied
Scientific EffectAerodynamic lift: Aerofoil

Implementation Method 2

striking the fixture (2) with the flying object (5), which causes the flying object (5) to rotate and decelerate

Methodology Applied
Scientific EffectImpact force: Impact Force

Data Source

PatentEP3835202B1Methods and apparatus to recover unmanned aerial vehicles (UAVS) with kites
Publication Date: 2024.03.13 INSITU INC
  • EP3835202B1 patent drawingFigure 1
  • EP3835202B1 patent drawingFigure 2A~2C
  • EP3835202B1 patent drawingFigure 3

AI summary

Methods and apparatus to recover unmanned aerial vehicles (UAVs) with kites are disclosed. A disclosed example apparatus to recover a UAV during flight includes a tether line, a tensioner operatively coupled to the tether line, and a kite operatively coupled to the tether line to support the tether line for recovery of the UAV.