Highly integrated man-portable anti-drone micro guidance device and control method

By integrating a main control module and multiple modules into a miniature anti-drone guidance device for individual soldiers, and adopting a DSP+FPGA architecture, the problems of low integration and slow response speed have been solved, realizing the miniaturization and rapid response of the device, and improving the strike accuracy and operational reliability.

CN122431213APending Publication Date: 2026-07-21SHANGHAI JIAO TONG UNIVERSITY INNER MONGOLIA RESEARCH INSTITUTE
View PDF 1 Cites 0 Cited by

Patent Information

Authority / Receiving Office
CN Β· China
Patent Type
Applications(China)
Current Assignee / Owner
SHANGHAI JIAO TONG UNIVERSITY INNER MONGOLIA RESEARCH INSTITUTE
Filing Date
2026-04-28
Publication Date
2026-07-21

AI Technical Summary

Technical Problem

Existing anti-drone guidance equipment suffers from low integration, heavy weight, slow response speed, and poor compatibility, making it difficult to meet the needs of individual soldier operations.

Method used

Design a highly integrated miniature guidance device for man-portable anti-UAVs, integrating a main control module, a target recognition and tracking module, a guidance sensing module, an actuator drive module, a laser fuse module, and a power supply module. Employ a DSP+FPGA heterogeneous architecture for data processing and control to achieve rapid startup and high-precision guidance.

Benefits of technology

It achieves miniaturization and lightweighting of equipment, rapid response capability, improved strike accuracy and operational reliability, supports power supply and parameter configuration for multiple scenarios, and simplifies the maintenance process.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN122431213A_ABST
    Figure CN122431213A_ABST
Patent Text Reader

Abstract

The application provides a highly integrated individual soldier anti-UAV micro guidance device and a control method, the device comprising a main control module, a target identification and tracking module, a guidance sensing module, an actuator driving module, a laser fuze module, a power supply module and an interface module integrated in the same shell; the main control module adopts a DSP+multi-FPGA heterogeneous operation architecture, the target identification and tracking module adopts a semi-active laser illumination and a linear array SPAD sensor, the guidance sensing module integrates a 6-axis IMU and a single-axis MEMS gyroscope, the actuator driving module drives a brushless DC steering engine and realizes steering engine rotation angle closed-loop control, and the laser fuze module realizes omnidirectional target detection and fuze trigger control through 3-way symmetrically arranged laser transceiving units. The application is adapted to individual soldier combat scenes and significantly improves anti-UAV strike precision and combat reliability.
Need to check novelty before this filing date? Find Prior Art