Wearable RPAS Controller with Relative Direction Indicator

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Solution Overview

Problem

Current remotely piloted aircraft systems (RPAS) controllers face challenges in accurately indicating the direction of the UAV to the pilot, especially at distances where the UAV becomes too small to discern its orientation, leading to difficulties in aligning and controlling the aircraft without clear visual cues.

Innovation Solution

The integration of a Relative Direction Indicator (RDI) on a graphical interface, combined with Pilot Compass Orientation and RDI-Align Function, utilizes GPS and compass data to provide the pilot with a graphical representation of the UAV's direction relative to their viewpoint, allowing for precise alignment and control through a smartphone interface.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If the UAV is operated at a distance beyond 100m, then the pilot's field of view is not obstructed and the UAV can operate freely, but the UAV becomes too small to discern its orientation and direction

Engineering Contradiction:
Improvepilot's field of viewVSAvoidUAV orientation discernibility
Core Design Contradiction:
Area of stationary objectVSMeasurement precision

Solution Approach 1:

The patent introduces an intermediary device (display screen showing RDI) between the pilot's visual observation and the UAV's actual orientation. The RDI acts as a mediator that translates the UAV's heading information into a visual representation on the display, allowing the pilot to discern orientation without needing to visually resolve the small UAV in the sky.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If the pilot moves or changes position, then the relative position to the UAV changes, but the pilot loses accurate knowledge of the UAV's direction relative to their new viewpoint

Engineering Contradiction:
Improvepilot mobilityVSAvoidUAV direction information
Core Design Contradiction:
Adaptability or versatilityVSLoss of information

Solution Approach 1:

The system implements feedback by continuously updating the RDI on the display based on the pilot's current position and orientation (obtained via GPS and compass) and the UAV's position. This closed-loop feedback ensures the RDI always accurately reflects the UAV's direction relative to the pilot's current viewpoint, maintaining orientation information even as the pilot moves.

Inventive Principle:
Principle #23Feedback

3Device complexity

If traditional visual cues alone are used to indicate UAV direction, then the system remains simple, but the pilot cannot accurately determine UAV orientation at distance

Engineering Contradiction:
Improveindication systemVSAvoidUAV direction indication
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The patent transitions from two-dimensional visual observation of the small UAV in the sky to a different dimensional representation - a graphical display showing the RDI. This dimensional change allows orientation information to be presented in a format that is easily interpretable regardless of the physical distance to the UAV.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

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

This solution enhances the controllability of RPAS by enabling pilots to accurately determine and align the UAV's direction, even at distances where visual cues are insufficient, improving safety and ease of operation by providing a clear graphical representation of the UAV's orientation relative to the pilot's viewpoint.

Implementation Method 1

a first position data from a satellite is received by a global navigation satellite system (GNSS) receiver

Methodology Applied
Scientific EffectSatellite positioning:

Implementation Method 2

an orientation of the controller is determined by a compass

Methodology Applied
Scientific EffectMagnetic field detection: Magnetic Field

Data Source

PatentEP3422129B1Controller for a remotely piloted aircraft system
Publication Date: 2019.06.19 DEUTSCHE TELEKOM AG
  • EP3422129B1 patent drawingFigure 1
  • EP3422129B1 patent drawingFigure 2
  • EP3422129B1 patent drawingFigure 3

AI summary

The disclosure relates to a controller (700) for a remotely piloted aircraft system (RPAS) (711), wherein the controller (700) is wearable by a pilot of the RPAS (711), the controller (700) comprising: a global navigation satellite system (GNSS) receiver (701), configured to receive first position data (702) from at least one satellite (712), the first position data (702) indicating a position of the controller (700); a communication interface (703) with the RPAS (711), configured to receive second position data (704) from the RPAS (711), the second position data (704) indicating a position of the RPAS (711); a compass (705) configured to provide orientation data (706) indicating an orientation of the controller (700) towards a geographical reference direction; a processor (707) configured to determine a relative direction (708) of the RPAS (711) towards the controller (700) based on the first position data (702), the second position data (704) and the orientation data (706); and a graphical interface (709) configured to provide a relative direction indicator (RDI) (710) providing a graphical indication of the relative direction (708) of the RPAS (711) towards the controller (700).