Gimbal Stabilized Radar for Remotely Operated Aerial Vehicles

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Solution Overview

Problem

Remotely operated aerial vehicles (ROAVs) face challenges in maintaining a consistent radar direction and elevation angle during changes in orientation, which affects their ability to effectively detect and avoid obstacles, especially in dynamic environments.

Innovation Solution

A gimbal stabilized radar system is mounted on a remotely operated aerial vehicle, allowing the radar unit to maintain a constant direction and elevation angle through multiple degrees of freedom, compensating for changes in pitch, roll, and yaw, ensuring continuous and accurate object detection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If the radar unit is mounted directly on the aerial vehicle without gimbal stabilization, then the device complexity is reduced, but the radar direction and elevation angle cannot be maintained constant during vehicle orientation changes

Engineering Contradiction:
Improveradar direction and elevation angle consistencyVSAvoidgimbal system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent applies dynamics by implementing a gimbal system with multiple degrees of freedom that allows the radar unit to dynamically adjust its orientation. The gimbal compensates for vehicle pitch, roll, and yaw movements through active mechanical adjustment, enabling the radar to maintain constant direction and elevation angles despite changes in vehicle orientation during flight operations.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The gimbal system serves as an intermediary between the aerial vehicle platform and the radar unit. It decouples the radar's directional stability from the vehicle's orientation changes, allowing the radar to maintain a stable viewing direction while the vehicle moves freely. This intermediary mechanism transfers and compensates for orientation disturbances without affecting the radar's measurement precision.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If the radar unit maintains constant direction and elevation angle through gimbal compensation, then obstacle detection accuracy is improved, but the device complexity and weight increase

Engineering Contradiction:
Improveobstacle detection accuracyVSAvoidgimbal stabilized radar system weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The dynamic gimbal system actively compensates for vehicle orientation changes to maintain constant radar direction and elevation angles. This dynamic adjustment ensures reliable obstacle detection accuracy by keeping the radar beam stabilized on target objects even during aggressive maneuvers or turbulent flight conditions.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The gimbal system provides multi-functionality by simultaneously compensating for multiple orientation parameters (pitch, roll, and yaw) with a single integrated mechanism. This universal approach to stabilization achieves reliable obstacle detection across various flight scenarios without requiring separate compensation systems for each orientation axis.

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

3Adaptability or versatility

If multiple degrees of freedom are provided in the gimbal system, then compensation for pitch, roll, and yaw changes is improved, but the device complexity increases

Engineering Contradiction:
Improvecompensation capability for orientation changesVSAvoidgimbal mechanism complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The multi-degree-of-freedom gimbal system provides dynamic compensation for pitch, roll, and yaw orientation changes. Each degree of freedom allows the radar unit to independently adjust for specific orientation disturbances, achieving comprehensive adaptability to various flight conditions while maintaining a manageable mechanical structure through coordinated motion control.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The gimbal system is segmented into multiple independent rotational axes, each handling specific orientation compensation tasks. This segmentation allows the complex problem of three-dimensional stabilization to be divided into manageable rotational components, where each axis compensates for specific pitch, roll, or yaw movements independently.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10409293B1Gimbal stabilized components for remotely operated aerial vehicles
Publication Date: 2019.09.10 EL-SIGHT LTD
  • US10409293B1 patent drawing
  • US10409293B1 patent drawing
  • US10409293B1 patent drawing

AI summary

The present invention extends to methods, systems, devices, apparatus, and computer program products for gimbal stabilized components for remotely operated vehicles. Aspects of the invention include a gimbal stabilized radar system. A radar unit is mounted on a vertical (or horizontal) gimbal attached to a remotely operated aerial vehicle. In aspects, a radar unit is mounted to a gimbal having multiple degrees of freedom. When the remotely operated aerial vehicle rotates and/or changes its orientation in space, the gimbal compensates keeping the direction and elevation angle of the radar essentially constant.