UAV Sensor-Guided Takeoff and Landing for Uneven Surfaces

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Solution Overview

Problem

Current methods for operating unmanned aerial vehicles (UAVs) require extensive practice and training, particularly for landing and takeoff, which can be challenging on uneven surfaces and in windy conditions.

Innovation Solution

The development of alternative methods for launching and decelerating UAVs, including detecting positional changes, visual signals, and release of a grip by a hand, to automatically activate the UAV's rotor blades and generate lift and/or thrust.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If traditional manual control methods are used for UAV takeoff and landing, then the UAV can be operated with basic control mechanisms, but the operation requires extensive practice and training especially on uneven surfaces and in windy conditions

Engineering Contradiction:
ImproveEase of takeoff and landing operationVSAvoidTime required for practice and training
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The UAV detects its own positional changes and environmental conditions using onboard sensors (accelerometers, gyroscopes, GPS) and automatically adjusts rotor blade pitch and motor speed to compensate for uneven surfaces and wind, enabling autonomous takeoff and landing without requiring operator skill or practice

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces manual mechanical control with an automated control system that uses sensor data (acceleration, orientation, position) to dynamically adjust rotor blade pitch angles and motor speeds, substituting the operator's manual interventions with automated electronic control algorithms

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

2Ease of operation

If automated detection and activation systems are implemented, then takeoff and landing become simpler for amateur users, but the device complexity increases with additional sensors and control mechanisms

Engineering Contradiction:
ImproveEase of takeoff and landing operationVSAvoidComplexity of sensors and control systems
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The onboard sensors serve multiple functions: accelerometers and gyroscopes detect both positional changes during takeoff/landing and orientation for navigation, GPS provides location data for both autonomous operation and telemetry, allowing the system to handle diverse operational requirements with a unified sensor suite

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The patent combines multiple sensor inputs (accelerometer, gyroscope, GPS) and control functions (rotor blade pitch adjustment, motor speed control) into an integrated autonomous control system that operates as a unified mechanism rather than separate independent systems

Inventive Principle:
Principle #5Merging (Combining)

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

These methods enable simplified and user-friendly UAV operation, allowing for successful takeoff and landing on uneven surfaces and in various environmental conditions, even for amateur users with little training.

Implementation Method 1

activating the UAV to generate a lift and/or thrust

Methodology Applied
Scientific EffectLift: Aerofoil

Implementation Method 2

activating the UAV to generate a lift and/or thrust

Methodology Applied
Scientific EffectThrust: Jet

Data Source

PatentUS12216479B2Methods for launching and landing an unmanned aerial vehicle
Publication Date: 2025.02.04 SZ DJI TECH CO LTD
  • US12216479B2 patent drawing
  • US12216479B2 patent drawing
  • US12216479B2 patent drawing

AI summary

An aerial vehicle landing method includes controlling to decelerate, with aid of one or more processors and in response to at least two of a plurality of conditions being satisfied, the aerial vehicle to cause the aerial vehicle to land autonomously. The plurality of conditions includes determining that an external signal related to a human is detected via one or more sensors; determining that a location/orientation change of the aerial vehicle is detected while the aerial vehicle is airborne; and determining that an external contact from an external object is exerted upon the aerial vehicle, the external object being an object that is not part of the aerial vehicle.