Hand Launchable UAV Targeting via Spiral Search and Sensor Feedback

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Solution Overview

Problem

Current unmanned aerial vehicles (UAVs) lack an efficient and precise targeting mechanism for guiding them to a desired target, particularly in a portable and user-friendly manner.

Innovation Solution

The design incorporates a body with lateral wings, flight control surfaces, and a propulsion system, along with an acquisition sensor and trigger sensor, allowing the UAV to search for and guide towards a target using a downward spiral path and activation mode, enabling precise targeting and potential responder activation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If current UAVs are used for reconnaissance and targeting, then they can perform basic flight and detection functions, but they lack efficient and precise targeting mechanisms for guiding to desired targets

Engineering Contradiction:
Improvetargeting precisionVSAvoidtargeting mechanism complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent implements feedback through the controller that receives signals from both the acquisition sensor (for target identification) and trigger sensor (for proximity detection), and automatically adjusts flight control surfaces to guide the UAV toward the target. This closed-loop feedback system enables precise automated targeting without requiring complex manual control mechanisms.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent replaces complex mechanical targeting mechanisms with sensor-based detection systems (acquisition sensor and trigger sensor) coupled with electronic flight control. This substitution of mechanical systems with sensor-electronic-control systems achieves precise targeting while reducing mechanical complexity.

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

2Ease of operation

If the UAV uses a portable launcher for deployment, then it achieves portability and ease of deployment, but it requires efficient targeting capabilities to compensate for limited launch control

Engineering Contradiction:
Improvedeployment easeVSAvoidtarget acquisition precision
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The patent employs preliminary action by equipping the UAV with pre-configured acquisition and trigger sensors that are ready to immediately detect and track targets upon deployment. The flight control system is pre-programmed with search and acquisition algorithms, enabling the UAV to quickly establish target contact without requiring complex pre-launch targeting preparations.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The UAV performs self-service targeting through its autonomous sensor systems that automatically detect, acquire, and track targets without external assistance. The trigger sensor autonomously determines proximity to targets and activates the responder, enabling the system to serve its own targeting needs efficiently.

Inventive Principle:
Principle #25Self-service

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 configuration enables the UAV to efficiently and accurately locate and engage targets, providing a portable and effective solution for reconnaissance and targeting applications.

Implementation Method 1

A propulsion device is operably coupled to the body

Methodology Applied
Scientific EffectThrust: Rocket

Implementation Method 2

A first flight control surface is supported by the body and is configured to control pitch of the vehicle. A second flight control surface is supported by the body and is configured to control yaw of the vehicle.

Methodology Applied
Scientific EffectAerodynamic force: Aerofoil

Implementation Method 3

The acquisition sensor includes a receiver directed downwardly from the body and is configured to identify a target

Methodology Applied
Scientific EffectElectromagnetic radiation detection: Radar

Implementation Method 4

The trigger sensor includes a receiver configured to detect proximity to a target

Methodology Applied
Scientific EffectProximity detection: Radar

Data Source

PatentUS8692171B2Hand launchable unmanned aerial vehicle
Publication Date: 2014.04.08 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY
  • US8692171B2 patent drawing
  • US8692171B2 patent drawing
  • US8692171B2 patent drawing

AI summary

An unmanned aerial vehicle including a controller operating in a search mode of operation where a receiver of an acquisition sensor searches for a target and causes flight control surfaces to guide the vehicle in a downward spiral path, a terminal mode of operation where the acquisition sensor detects a target and causes flight control surfaces to direct the vehicle toward the target, and an activation mode of operation where a trigger sensor detects a target within a predetermined distance to the vehicle and the controller activates a responder.