Gimbal Stabilized Camera for Drone Hovering Stability

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Solution Overview

Problem

Unmanned electronic devices, such as drones, face challenges in maintaining a stable hovering state due to external factors like wind and propeller operation, leading to tilting and inaccurate flight control signals, which result in unnecessary movements and energy consumption.

Innovation Solution

An electronic device equipped with a gimbal, multiple cameras, and sensors that use processors to detect changes in angle and maintain camera horizontality, compensating for tilts and adjusting flight controls to stabilize hovering without unnecessary movements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the OFS module is mounted on the bottom surface to detect ground points for hovering control, then the hovering function is enabled, but the module tilts with the airframe causing inaccurate position identification and unnecessary flight corrections

Engineering Contradiction:
Improvehovering stabilityVSAvoidpoint of interest detection accuracy
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The patent separates the OFS module from the airframe by mounting it on an independently controllable support structure (such as a gimbal or extended arm). This segmentation allows the OFS module to maintain a fixed orientation relative to the ground while the airframe tilts, resolving the contradiction between enabling hovering control and maintaining detection accuracy.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces an intermediary mechanism (such as a gimbal system or adjustable mounting structure) between the airframe and the OFS module. This intermediary compensates for airframe tilting by actively adjusting the OFS module's orientation to remain horizontal, thereby maintaining accurate ground point detection while preserving hovering functionality.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Extent of automation

If flight control signals are generated to return to original position based on tilted OFS module data, then the control system responds to detected movements, but unnecessary operations are performed when the device is actually stationary

Engineering Contradiction:
Improveautomatic flight controlVSAvoidenergy consumption from unnecessary operations
Core Design Contradiction:
Extent of automationVSLoss of energy

Solution Approach 1:

The patent implements a feedback mechanism where the orientation of the OFS module is continuously monitored and used to validate position changes. By ensuring the OFS module remains horizontal through active compensation, the system receives accurate feedback about actual ground position changes, enabling the automatic flight control to distinguish between real drift and apparent movement caused by tilting, thus avoiding unnecessary energy-consuming corrections.

Inventive Principle:
Principle #23Feedback

3Adaptability or versatility

If the airframe tilts due to external factors during hovering, then the device adapts to external forces, but the mounted OFS module tilts causing measurement errors

Engineering Contradiction:
Improveresponse to external factorsVSAvoidOFS module measurement accuracy
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The patent employs a counterbalancing mechanism where the support structure for the OFS module actively compensates for tilting forces. When external factors cause the airframe to tilt, the support structure generates opposing adjustments to maintain the OFS module in a horizontal position, effectively neutralizing the harmful effect of airframe tilting on measurement accuracy while preserving the ability to adapt to external conditions.

Inventive Principle:
Principle #8Anti-weight (Counterweight)

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 effectively maintains stable hovering and reduces energy consumption by accurately identifying point changes on the ground, preventing unnecessary flights and ensuring a constant image capture.

Implementation Method 1

detect a change in an angle of the electronic device by a sensor

Methodology Applied
Scientific EffectGravitation: Gravitation

Implementation Method 2

control hovering of the electronic device using a first motor for a thrust related to a flight of the electronic device

Methodology Applied
Scientific EffectThrust: Force

Data Source

PatentUS10054946B2Electronic device and operating method thereof
Publication Date: 2018.08.21 SAMSUNG ELECTRONICS CO LTD
  • US10054946B2 patent drawing
  • US10054946B2 patent drawing
  • US10054946B2 patent drawing

AI summary

An electronic device is provided. The electronic device includes a gimbal; a first camera; a second camera to detect a point of interest on ground; at least one sensor; a first motor; a second motor to operate the first camera and the second camera to maintain horizontality; and at least one processor electrically connected to the first camera, the second camera, the at least one sensor, the first motor, and the second motor, wherein the at least one processor is configured to detect a change in an angle; control the second motor to control the second camera to maintain horizontality; determine whether the point of interest is changed; if the point of interest is not changed, control the first motor to maintain hovering; and, if the point of interest is changed, control the first motor to maintain hovering by moving to original position before moving and compensating for tilt.