UAV Obstacle Avoidance Control for Low-Altitude Flight Flexibility

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Solution Overview

Problem

Unnecessary restriction of unmanned aerial vehicle flight due to collision avoidance functions, particularly during takeoff, landing, or low altitude operations.

Innovation Solution

A control device for unmanned aerial vehicles that disables the obstacle avoidance function when specific conditions are met, such as a tilt angle exceeding a threshold, during takeoff or landing, or when the altitude is below a certain height, thereby preventing false obstacle detection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the obstacle avoidance function is always enabled, then collision safety is improved, but flight operation flexibility deteriorates due to unnecessary restrictions during takeoff, landing, and low altitude operations

Engineering Contradiction:
Improvecollision safetyVSAvoidflight operation flexibility
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The obstacle avoidance function is made dynamically controllable through a disablement determination unit that adjusts its activation state based on flight conditions. The system transitions from a static always-on state to a dynamic state that adapts to operational context, disabling the function when ground detection is likely (during takeoff, landing, low altitude, or high tilt angle operations) and enabling it during normal flight, thereby resolving the contradiction between safety and operational flexibility

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the operational parameter of the obstacle avoidance function from a fixed enabled state to a variable state based on flight parameters. By monitoring parameters such as altitude, tilt angle, and flight phase (takeoff/landing), the system adjusts whether the obstacle avoidance function is active, allowing optimal balance between collision prevention and operational freedom across different flight scenarios

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If the obstacle avoidance function is enabled at low altitude, then obstacle detection capability is improved, but false detection of ground increases causing unnecessary flight restriction

Engineering Contradiction:
Improveobstacle detection capabilityVSAvoidfalse obstacle detection
Core Design Contradiction:
Measurement precisionVSObject-generated harmful factors

Solution Approach 1:

A ground detection unit acts as an intermediary between the obstacle sensor and the obstacle avoidance function. This intermediary layer analyzes whether detected objects are actually ground or true obstacles by considering flight phase and altitude context, preventing false ground detection from triggering unnecessary obstacle avoidance maneuvers while maintaining accurate obstacle detection capability when needed

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If the obstacle avoidance function restricts flight to avoid potential collisions, then safety is improved, but operational efficiency deteriorates during normal flight operations

Engineering Contradiction:
Improveflight safetyVSAvoidoperational efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The obstacle avoidance function operates dynamically rather than statically, being enabled only when flight conditions warrant caution (normal flight at sufficient altitude) and disabled when operations require freedom of movement (takeoff, landing, low altitude work). This dynamic adjustment maintains safety during vulnerable phases while preserving operational efficiency during routine operations

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP4620804A1Unmanned aerial vehicle, unmanned aerial vehicle control system, and unmanned aerial vehicle control method
Publication Date: 2025.09.24 KUBOTA CORP
  • EP4620804A1 patent drawingFigure 1A
  • EP4620804A1 patent drawingFigure 1B
  • EP4620804A1 patent drawingFigure 1C

AI summary

A control device for a multicopter has an obstacle avoidance function to detect an obstacle based on a signal output from the obstacle sensor and to perform operations to avoid collision with the obstacle. The control device disables the obstacle avoidance function when a predetermined condition is satisfied, and enables the obstacle avoidance function when the predetermined condition is not satisfied. The predetermined condition includes at least one of: a first condition that a tilt angle of the body is greater than a predetermined angle; a second condition that the unmanned aerial vehicle is in a takeoff operation or a landing operation; or a third condition that an altitude of the body is at or below a predetermined height.