Flight Power Supply Control for Optical Charging of Solar UAVs

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Solution Overview

Problem

Existing technologies face challenges in efficiently transmitting power to high-altitude platforms like stratospheric platforms, particularly due to the need for high-precision tracking and the impact of weather conditions such as clouds.

Innovation Solution

A control device is used to control a power supply flight vehicle, which follows the flight of a power supply target flight vehicle equipped with a solar cell panel. The control device includes a light irradiation unit that radiates light towards the solar cell panel, with the direction of the light adjusted based on the posture and movement of the target flight vehicle to optimize power generation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If light is radiated from the ground to the high-altitude platform, then power transmission can be achieved, but the transmission efficiency is reduced due to weather conditions such as clouds

Engineering Contradiction:
Improvepower transmission efficiencyVSAvoidweather conditions impact
Core Design Contradiction:
Loss of energyVSObject-affected harmful factors

Solution Approach 1:

A flight vehicle equipped with solar cell panels serves as an intermediary carrier between the ground-based light source and the power reception system. The flight vehicle flies through the atmosphere to collect light energy, avoiding direct ground-to-platform transmission through cloudy regions, thereby reducing energy loss and weather-related interference.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Power

If ground-based laser irradiation is used for power transmission, then power supply to high-altitude platforms is enabled, but high-precision tracking is required which increases system complexity

Engineering Contradiction:
Improvepower transmission capabilityVSAvoidtracking system complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The system employs dynamic tracking where the flight vehicle actively adjusts its position and orientation in real-time to maintain optimal alignment with the ground-based laser source. This dynamic adaptation simplifies the overall tracking requirement compared to a static high-altitude platform, as the mobile platform can more easily follow the laser beam movement.

Inventive Principle:
Principle #15Dynamics

3Loss of energy

If the flight vehicle follows the target flight vehicle closely, then weather impact is reduced, but the control system complexity increases

Engineering Contradiction:
Improvepower reception efficiencyVSAvoidcontrol system complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The control system implements feedback mechanisms where the flight vehicle continuously monitors its position relative to the target flight vehicle and adjusts its flight path accordingly. This feedback-based control ensures the flight vehicle maintains optimal positioning for light collection while managing control complexity through automated closed-loop regulation.

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

This solution enables efficient power transmission to high-altitude platforms by maintaining the power supply flight vehicle in close proximity to the target flight vehicle, thereby reducing the impact of weather conditions and ensuring high-precision tracking.

Implementation Method 1

a light irradiation unit 112 that radiates light 120 toward the solar cell panel 330

Methodology Applied
Scientific EffectPhotovoltaic Effect: Photovoltaic Effect

Data Source

PatentEP4269241B1Control device, program, system, and control method
Publication Date: 2025.01.29 SOFTBANK CORPORATION
  • EP4269241B1 patent drawingFigure 1
  • EP4269241B1 patent drawingFigure 2
  • EP4269241B1 patent drawingFigure 3

AI summary

Provided is a control device that controls a power supply flight vehicle, the control device including a control unit which controls the power supply flight vehicle so as to cause a light irradiation unit to radiate light toward a solar cell panel while flying following flight of a power supply target flight vehicle on which the solar cell panel is mounted. Provided is a control method to control a power supply flight vehicle, which is executed by a computer, the control method including controlling the power supply flight vehicle so as to cause a light irradiation unit to radiate light toward a solar cell panel while flying following flight of a power supply target flight vehicle on which the solar cell panel is mounted.