UAV Controller Cover With Integrated Antennas and RF Shielding

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Solution Overview

Problem

Unmanned aerial vehicle (UAV) controllers are vulnerable to environmental conditions, such as breaking from drops and overheating, and their control elements and antennas are susceptible to damage and interference, affecting communication and accuracy.

Innovation Solution

A clamshell cover integrates antennas and control elements, providing protection and improved RF communication by angling antennas towards the UAV, with a conductive plane to direct RF energy and insulating plane to isolate it from the user, along with a heatsink and fan for cooling and a support mechanism for stability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If control elements and antennas are exposed for operation, then ease of operation and communication are improved, but vulnerability to damage from drops and environmental conditions increases

Engineering Contradiction:
Improveaccessibility of control elementsVSAvoidprotection from damage
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The cover is designed to be movable between open and closed positions, allowing the controller to dynamically adapt its protection level based on operational needs. When open, control elements are accessible for operation; when closed, they are protected from damage.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The controller is divided into separate functional sections: a movable cover containing control elements and antennas, and a base containing inertial measurement units and other sensitive circuitry. This segmentation allows each part to be optimized independently for its specific function.

Inventive Principle:
Principle #1Segmentation

2Reliability

If antennas are positioned for optimal RF communication, then communication range is improved, but susceptibility to interference and damage increases

Engineering Contradiction:
ImproveRF communication rangeVSAvoidsusceptibility to interference and damage
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The antennas are integrated into the movable cover, allowing their position to be dynamically adjusted. When the cover is opened for operation, antennas are positioned for optimal communication; when closed, they are protected within the cover structure.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

A conductive plane is introduced as an intermediary between the antennas and the environment. This conductive plane directs RF energy toward the UAV while blocking external interference, serving as a protective mediator that maintains communication effectiveness while reducing susceptibility to harmful factors.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If control elements are made robust for durability, then protection from damage is improved, but accuracy of inertial measurement units may be affected by mechanical stress

Engineering Contradiction:
Improvedurability of control elementsVSAvoidaccuracy of IMUs
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The controller is segmented into a cover section containing robust control elements and a base section containing sensitive IMUs. This physical separation prevents mechanical stress from durable control elements from affecting IMU accuracy.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The movable cover acts as an intermediary structure that isolates the IMUs from direct mechanical stress. The cover can be opened and closed without transmitting significant force to the IMUs in the base, protecting measurement precision while allowing durable control elements.

Inventive Principle:
Principle #24Intermediary (Mediator)

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

Enhances protection of control elements and antennas, improves RF communication range, and maintains accuracy of inertial measurement units (IMUs) by isolating sensitive circuitry, thus enhancing the durability and performance of the UAV controller.

Implementation Method 1

a conductive plane to direct RF energy

Methodology Applied
Scientific EffectElectromagnetic radiation directionality: Electromagnetic Induction

Implementation Method 2

an insulating plane to isolate it from the user

Methodology Applied
Scientific EffectElectromagnetic shielding: Faraday Cage

Implementation Method 3

a heatsink and fan for cooling

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 4

a heatsink and fan for cooling

Methodology Applied
Scientific EffectForced convection: Forced Convection

Data Source

PatentUS12449805B2Unmanned aerial vehicle (UAV) controller
Publication Date: 2025.10.21 SKYDIO INC
  • US12449805B2 patent drawing
  • US12449805B2 patent drawing
  • US12449805B2 patent drawing

AI summary

An apparatus that includes a controller of an unmanned aerial vehicle (UAV), a cover, and antennas integrated into the cover and electrically connect to circuitry of the controller. The controller includes control elements configured to receive inputs. The cover is coupled to the controller and movable between a closed position, in which the control elements are covered, and an open position in which the control elements are exposed. The cover includes one or more ribs integrated into an interior surface of the cover and defining cavities of the cover. The cover also includes a conductive plane coupled to the one or more ribs that encloses the cavities.