Gravity-Guided Kinetic Projectile Steering for Precise Aerial Delivery

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Solution Overview

Problem

Current weapon delivery systems from aerial vehicles lack precision and efficiency in guiding kinetic projectiles without onboard propulsion or explosive materials, relying on complex guidance systems and requiring costly and heavy guidance components.

Innovation Solution

A projectile delivery module for aerial vehicles that uses gravity-driven kinetic projectiles with onboard steering systems, controlled by a base system including a target tracking and guidance system, eliminating the need for onboard propulsion and explosive materials, and leveraging computer vision and RF communication for precise targeting.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If kinetic projectiles use complex onboard guidance systems, then targeting precision is improved, but device complexity and cost increase

Engineering Contradiction:
Improvetargeting precisionVSAvoidguidance system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent extracts the guidance computations from the projectile itself and relocates them to the base system on the aerial vehicle. The projectile only carries minimal steering components while the base system performs all complex tracking and guidance calculations, significantly reducing onboard projectile complexity while maintaining precision

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent merges the target tracking, projectile tracking, and guidance computation functions into a single integrated base system. This consolidation eliminates the need for separate complex guidance systems on each projectile while achieving the same or better precision through centralized control

Inventive Principle:
Principle #5Merging (Combining)

2Speed

If kinetic projectiles carry onboard propulsion mechanisms, then flight control capability is improved, but weight and device complexity increase

Engineering Contradiction:
Improveflight control capabilityVSAvoidprojectile weight
Core Design Contradiction:
SpeedVSWeight of moving object

Solution Approach 1:

The patent removes onboard propulsion mechanisms from the projectiles entirely. Instead, the base system provides all necessary thrust and propulsion control, allowing projectiles to remain lightweight while maintaining full flight control capability through external actuation

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The base system acts as an intermediary that provides propulsion and flight control functions to the projectiles without being physically integrated into them. This allows projectiles to remain simple, lightweight objects while the base system mediates all complex flight control operations

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If kinetic projectiles carry explosive materials, then target engagement effectiveness is improved, but harmful factors and safety risks increase

Engineering Contradiction:
Improvetarget engagement effectivenessVSAvoidcollateral damage
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent converts the traditional explosive engagement method into a kinetic impact method. Instead of using explosives that create widespread destruction, the system uses precisely controlled kinetic projectiles that deliver focused impact energy, reducing collateral damage while maintaining or improving target engagement effectiveness through precision

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

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

Enables precise and efficient delivery of kinetic projectiles to targets using gravity, reducing collateral damage and operational costs by simplifying the projectile design and shifting guidance computations to the base system, enhancing the operational endurance of the weaponized aerial vehicle.

Implementation Method 1

release the kinetic projectile from the projectile holder such that the kinetic projectile is driven toward a target by gravity

Methodology Applied
Scientific EffectGravity: Gravitation

Implementation Method 2

a steering mechanism operable to change an attitude, orientation, and/or direction of flight of the kinetic projectile

Methodology Applied
Scientific EffectAerodynamic force: Aerofoil

Data Source

PatentUS11685527B2Projectile delivery systems and weaponized aerial vehicles and methods including same
Publication Date: 2023.06.27 CORVID TECHNOLOGIES LLC
  • US11685527B2 patent drawing
  • US11685527B2 patent drawing
  • US11685527B2 patent drawing

AI summary

A projectile delivery module to be mounted on an aerial vehicle includes a projectile delivery system including a kinetic projectile and a base system. The kinetic projectile includes a projectile body, an RF receiver, and an onboard steering system including: a steering mechanism operable to change an attitude, orientation, and/or direction of flight of the kinetic projectile; and a steering actuator. The base system includes: an RF transmitter to communicate with the RF receiver; a projectile holder; a target tracking system; and a projectile guidance system including a projectile tracking system and a projectile control system. The base system is configured to: release the kinetic projectile from the projectile holder such that the kinetic projectile is driven toward a target by gravity; track the target using the target tracking system; track the released kinetic projectile using the projectile tracking system; and automatically control the onboard steering system using the projectile control system to adjust a trajectory of the falling kinetic projectile to steer the kinetic projectile to the target.