Intelligent Munition Flight Control via Drag Mechanisms
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Solution Overview
Problem
Conventional non-lethal munitions suffer from inaccuracy and short range, failing to reliably disable targets from a distance due to limitations in electronics and flight control systems.
Innovation Solution
An intelligent munition system that incorporates a control section with drag mechanisms and electrode deployment, using on-board circuitry to adjust flight characteristics and deploy electrodes for optimal non-lethal impact, enabling accurate and long-range disabling of targets.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If conventional non-lethal munitions are used, then the munition structure is simple, but the accuracy and range are limited
Solution Approach 1:
The munition is divided into distinct functional segments: a control section containing electronics and drag mechanisms, and a deployment section containing electrodes. This segmentation allows each component to be optimized independently, enabling advanced flight control and accurate target engagement while maintaining a manageable overall structure that fits within conventional firearm constraints.
Solution Approach 2:
The munition incorporates dynamic drag mechanisms that can be activated during flight to alter flight characteristics. This dynamic adjustment capability enables real-time correction of trajectory and speed, significantly improving accuracy and extending effective range while keeping the base structure relatively simple.
2Length of stationary object
If conventional non-lethal munitions are used, then the munition is easy to manufacture, but the range is short
Solution Approach 1:
Drag mechanisms are pre-positioned within the munition structure during manufacturing, but remain inactive until needed during flight. This preliminary preparation allows the munition to maintain a compact, easy-to-manufacture form while gaining extended range capability through later activation of the drag mechanisms to control descent and prolong flight time.
3Ease of operation
If drag mechanisms are added to control flight, then the flight characteristic control is improved, but the device complexity increases
Solution Approach 1:
The control electronics are integrated directly into the munition, allowing it to autonomously control its own flight characteristics. The system self-regulates by activating drag mechanisms based on embedded control logic, eliminating the need for complex external control systems while maintaining ease of operation through automatic flight adjustment.
4Reliability
If electronics are incorporated for intelligent control, then the target disabling capability is improved, but the manufacturing complexity increases
Solution Approach 1:
The control electronics serve multiple functions: managing drag mechanism activation, controlling electrode deployment timing, and coordinating overall munition operation. This multi-functionality reduces the total number of separate components needed, simplifying manufacturing while maintaining reliable intelligent control for accurate target disabling.
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
The system provides reliable, accurate, and efficient non-lethal disabling of targets at extended ranges by intelligently controlling the flight and deployment of electrodes, overcoming the limitations of conventional munitions.
Implementation Method 1
Firing the munition case from a firearm propels the load from the munition case and a barrel of the firearm towards a target
Implementation Method 2
The drag mechanism alters a flight characteristic of the load
Data Source
AI summary
A small arms form factor munition may package a control section with a deployment section in a munition case. The control section can have a first drag mechanism and a second drag mechanism. Firing the munition case from a firearm propels the load from the munition case and barrel of the firearm towards a target. A drag mechanism is selected and activated by the control section in response to a detected distance to the target while the load is in flight. The drag mechanism alters a flight characteristic of the load.