Aircraft Vision Positioning in Low-Light via Adaptive Illumination

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Solution Overview

Problem

Aircrafts face difficulties in effectively performing vision positioning and control in low-light environments, leading to potential accidents during landing or hovering due to insufficient ambient luminance, which impairs the functionality of vision systems.

Innovation Solution

An aircraft control method and apparatus that utilize a luminance sensing apparatus to determine ambient luminance levels and adjust the working status of a light emitting apparatus to ensure the vision system operates within a required luminance range, enhancing visibility and control capabilities.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If the aircraft uses a vision auxiliary apparatus to obtain flight environment information, then the aircraft can implement precise hovering and intelligent landing and obstacle avoidance, but in low-light environments the vision positioning cannot be effectively performed

Engineering Contradiction:
Improvevision positioning accuracyVSAvoidambient luminance
Core Design Contradiction:
Measurement precisionVSIllumination intensity

Solution Approach 1:

The patent introduces a light emitting apparatus as an intermediary device to illuminate the flight environment. This mediator provides additional light to the scene being observed by the vision system, enabling effective vision positioning in low-light conditions without directly modifying the vision apparatus itself

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent changes the lighting parameters of the flight environment by controlling the light emitting apparatus to emit light with specific intensity and duration. This parameter change transforms the ambient luminance from insufficient to adequate levels, enabling the vision system to function properly

Inventive Principle:
Principle #35Parameter changes

2Use of energy by moving object

If the aircraft operates in low-light environments without additional lighting, then energy consumption is reduced, but the vision system cannot run normally and the aircraft cannot learn the flight environment

Engineering Contradiction:
Improveenergy consumptionVSAvoidvision system functionality
Core Design Contradiction:
Use of energy by moving objectVSReliability

Solution Approach 1:

The patent implements dynamic control of the light emitting apparatus based on real-time assessment of ambient luminance and vision system performance. The lighting is activated only when needed (when ambient light is insufficient), and adjusted in intensity and duration to provide minimum necessary illumination, optimizing the balance between energy consumption and vision system reliability

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent employs feedback mechanisms where the vision system's performance is continuously monitored, and this information feeds back to control the light emitting apparatus. When the vision system detects insufficient lighting conditions, it triggers the light emitting apparatus to provide additional illumination, creating a closed-loop control system that adapts to environmental conditions

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

The solution enables effective vision positioning and convenient control of aircrafts in low-light conditions by adjusting light emitting apparatuses to meet the necessary luminance requirements for the vision system, preventing accidents and ensuring safe operations.

Implementation Method 1

obtaining, by a luminance sensing apparatus of an aircraft, ambient luminance data

Methodology Applied
Scientific EffectLuminance detection: Photoelectric Effect

Implementation Method 2

adjusting a working status of a light emitting apparatus on the aircraft

Methodology Applied
Scientific EffectLight emission: Light Emitting Diode

Data Source

PatentUS11136138B2Aircraft control method and apparatus and aircraft
Publication Date: 2021.10.05 AUTEL ROBOTICS CO LTD
  • US11136138B2 patent drawing
  • US11136138B2 patent drawing
  • US11136138B2 patent drawing

AI summary

This invention discloses an aircraft control method, apparatus and an aircraft. The invention relates to the field of aircraft control technologies. The method includes: obtaining ambient luminance data by a luminance sensing apparatus of an aircraft; determining whether the ambient luminance data satisfies a luminance value required for normal running of a vision system of the aircraft; and adjusting, when the ambient luminance data does not satisfy the luminance value required for normal running of the vision system of the aircraft, a working status of a light emitting apparatus on the aircraft to change light emitting luminance of the light emitting apparatus. The foregoing aircraft control method, apparatus and the aircraft can accurately learn a flight environment in which the aircraft is located, thereby effectively implementing vision positioning on the aircraft and more conveniently controlling the aircraft.