UAV Power-Up Sequence With Remote Arming and Startup Delay

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Solution Overview

Problem

Unmanned aerial vehicles (UAVs) often require physical interaction for power-up, posing safety risks due to the need for ground crew proximity during startup, and existing systems lack controlled power-up sequences to prevent accidental activation.

Innovation Solution

A power sequence control system communicatively coupled to a remote user terminal, which electrically couples a battery to the propulsion system only after a user-operated switch is toggled and a power-on signal is received, incorporating visual and audio indications for sequence status and incorporating delays to ensure ground crew safety.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If physical interaction with ground crew is required for power-up, then the UAV can be powered on, but safety risks increase due to ground crew proximity requirements

Engineering Contradiction:
ImprovesafetyVSAvoidoperational complexity
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The patent replaces the mechanical/physical interaction system (ground crew manually switching) with an electronic/wireless communication system. The power-up sequence is controlled through wireless signals from a remote terminal, eliminating the need for ground crew physical proximity to the UAV during startup.

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

Solution Approach 2:

The patent introduces a remote terminal as an intermediary between the operator and the UAV power-up system. This intermediary enables power-up control from a distance, removing the need for direct physical contact with the UAV while maintaining controlled activation.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of operation

If simple power-up switching is used, then ease of operation is maintained, but accidental activation probability increases

Engineering Contradiction:
ImprovesimplicityVSAvoidaccidental activation prevention
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The patent segments the power-up process into distinct sequential stages: initial power application, system initialization, and operational mode activation. This segmentation ensures that power is applied in a controlled sequence rather than all at once, reducing accidental full activation while maintaining operational simplicity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent implements preliminary actions before full power activation, including a power-up sequence that initializes systems gradually and requires confirmation steps. This preliminary action framework prevents accidental full power-on while keeping the interface simple for legitimate users.

Inventive Principle:
Principle #10Preliminary action

3Productivity

If rapid power-up is implemented, then productivity is improved, but safety risks increase due to insufficient ground crew clearance time

Engineering Contradiction:
Improvepower-up speedVSAvoidground crew safety
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The patent implements a preliminary delay period in the power-up sequence that allows ground crew to clear the area before full power is applied. This preliminary action maintains rapid overall power-up while ensuring safety clearance, resolving the contradiction between speed and safety.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP3974324B1A controlled powerup sequence for an unmanned aerial vehicle (UAV)
Publication Date: 2023.10.25 INSITU INC
  • EP3974324B1 patent drawingFigure 1
  • EP3974324B1 patent drawingFigure 2
  • EP3974324B1 patent drawingFigure 3

AI summary

A controlled power up sequence for an unmanned aerial vehicle (UAV) is disclosed. A disclosed example controlled power up sequence for a UAV (102) includes a remote user terminal (106), and a power sequence control interface (104) including a transceiver (218) communicatively coupled to the remote user terminal, a user-operated switch (204) of the UAV, and a power controller (308) to electrically couple a power source of the UAV to a propulsion system (216) of the UAV in response to the user-operated switch being toggled on and the power sequence control interface receiving, via the transceiver, a power on signal from the remote user terminal.