UAV Take-off Control via Vertical Velocity Feedback

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Solution Overview

Problem

Current UAV take-off methods require skilled operators to manage attitude balance and propulsion power, especially during hand launching, which can be hazardous and inefficient.

Innovation Solution

A method and apparatus for controlling UAVs that involve receiving a take-off preparatory signal, controlling rotor speed from idle to rated speed based on predetermined conditions, allowing the UAV to hover and stabilize autonomously, reducing operator skill requirements and enhancing safety.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If hand launching is used to lower operator skill requirements, then ease of operation is improved, but safety deteriorates due to hazardous conditions

Engineering Contradiction:
Improveoperator skill requirementVSAvoidtake-off safety
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The UAV autonomously controls its own take-off process by detecting vertical velocity and automatically adjusting rotor speed, eliminating the need for operator intervention during the critical take-off phase. The system serves itself by making independent decisions about when to increase power and how to maintain stability.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The control system continuously monitors vertical velocity and uses this feedback to dynamically adjust rotor speed. The detector provides real-time information about upward motion, and the controller responds by modulating motor power to maintain safe and stable take-off conditions.

Inventive Principle:
Principle #23Feedback

2Reliability

If professional users manually control take-off, then safety is improved through skilled operation, but ease of operation deteriorates due to high skill requirements

Engineering Contradiction:
Improvetake-off safetyVSAvoidoperator skill requirement
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The UAV autonomously controls its own take-off process by detecting vertical velocity and automatically adjusting rotor speed, eliminating the need for operator intervention during the critical take-off phase. The system serves itself by making independent decisions about when to increase power and how to maintain stability.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces manual mechanical control by the operator with an automated electronic control system that uses sensors to detect vertical velocity and electronically adjusts motor speed, substituting human skill with automated detection and control mechanisms.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Productivity

If rotor speed is increased rapidly for quick take-off, then productivity is improved, but reliability deteriorates due to loss of attitude balance

Engineering Contradiction:
Improvetake-off speedVSAvoidattitude balance
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The control system dynamically adjusts rotor speed based on real-time vertical velocity detection rather than using a fixed rapid acceleration profile. The system adapts the power increase rate to actual flight conditions, allowing fast take-off when conditions permit while maintaining balance when needed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The control system continuously monitors vertical velocity and uses this feedback to dynamically adjust rotor speed. The detector provides real-time information about upward motion, and the controller responds by modulating motor power to maintain safe and stable take-off 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

Enables safe and efficient UAV take-off with reduced operator expertise, as the UAV can autonomously adjust its vertical velocity and propulsion to achieve stable hovering and normal flight states.

Implementation Method 1

at least one rotor... controlling a rotation speed of the at least one rotor... increasing the rotation speed of the at least one rotor

Methodology Applied
Scientific EffectNewton's Third Law (Action-Reaction): Reaction (physics)

Data Source

PatentUS9632501B1Method and apparatus for controlling UAV, and UAV take-off system
Publication Date: 2017.04.25 ZEROTECH (SHENZHEN) INTELLIGENCE ROBOT CO LTD
  • US9632501B1 patent drawing
  • US9632501B1 patent drawing
  • US9632501B1 patent drawing

AI summary

A method for controlling an unmanned aerial vehicle (UAV) is provided. The UAV comprises at least one rotor. The method includes receiving a take-off preparatory signal; controlling a rotation speed of the at least one rotor with an idle speed rotation in response to the take-off preparatory signal; increasing the rotation speed of the at least one rotor up to a rated speed rotation under predetermined conditions.