DIGITRON ㈜디지트론
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Guided Weapons

Centred on the guidance & control unit, Digitron develops and produces the core electronics of guided-weapon systems — guidance data receivers, actuation controllers, anti-jam GNSS RF assemblies, fuze TDD signal processors, and seeker frequency synthesizers and servo controllers. We also supply the command & communication device and code loader that support weapon employment, and guidance & control units for aerial target drones.

Guidance & Control Unit (GCU)

The brain of the round: it links the forward subsystems — seeker, IMU, guidance data receiver — with the aft subsystems — actuation unit, anti-jam GNSS, fuze — and controls every phase of flight.

Operating Concept

Guidance & Control Unit — Operating Concept

Inside a guided-weapon system the guidance & control unit exchanges power, commands and target data with the forward and aft subsystems, controlling the round through every phase of flight. The diagram magnifies the position of the unit within the round and shows the signals exchanged with each subsystem.

Guidance & Control Unit
Forward Subsystems
Nose Cap
  • Incoming signalNose-cap separation signal
  • Incoming signalPower, target data, commands
  • Outgoing signalTarget data, track & detection data
Inertial Measurement Unit
  • Outgoing signalAcceleration, angular rate
  • Incoming signalPower, clock
  • Incoming signalPower, commands
  • Outgoing signalTarget data, mission data
Aft Subsystems
  • Two-way signalDrive commands, responses, status
  • Incoming signalPower
  • Outgoing signalGNSS data, status
  • Incoming signalPower, commands
Flight Measurement Unit
  • Incoming signalIn-round data, power
  • Incoming signalDetonation signal, delay data
  • Outgoing signalStatus data
Guided-rocket configuration — the marked band is where the guidance & control unit sits

Guided-rocket configuration — the marked band is where the guidance & control unit sits

130 mm Guided Rocket-Ⅱ Guidance & Control Unit

01
  • High-performance computing and control

    DSP- and FPGA-based data-processing architecture and memory system

  • Multiple communication interfaces

    High-speed, high-reliability interfaces across serial, industrial-network and Ethernet standards

  • Signal processing and circuit design

    Multi-channel signal-control circuits with FPGA-integrated communication channels

  • System health monitoring and protection

    Real-time temperature and voltage monitoring, with protection circuits for discrete I/O signals

EA Guidance & Control Unit (Export)

In production
  • High-performance control and data processing

    DSP- and FPGA-based digital signal processing and memory control

  • Reliable communication interfaces

    Industrial CAN and multi-channel serial (RS-422) communication modules

  • Hardware optimisation

    Multiple PCBs integrated into a single board for maximum space efficiency and productivity

  • Commercial results

    Development completed and series production established

L-SA* Guidance & Control Unit

03
  • High-performance computing and control processing

    DSP- and FPGA-based data-processing architecture with a high-speed memory system

  • Multiple communication interfaces

    Reliable communication modules for serial (RS-422, UART), Ethernet and CAN

  • Signal control and logic design

    Multi-channel signal-control circuits with FPGA-integrated communication channels

  • Health monitoring and circuit protection

    Real-time temperature and voltage monitoring, with protection circuits for discrete I/O signals

REDEYE Guidance & Control Unit (Export)

04
  • Thermal management and reliability

    Heat-dissipation design for efficient heat spreading and thermal management

  • Multiple communication interfaces

    Wired and high-speed communication control across a range of standard interfaces

  • Signal processing and logic design

    Multi-channel signal-control circuits with communication channels integrated in programmable logic

  • Real-time monitoring interface

    Real-time temperature and voltage-level sensing to track system status

  • Signal control and circuit protection

    Discrete-signal I/O control and protection circuits for system stability

Ship-** Ⅱ Guidance & Control Unit

05
  • Thermal management and heat-dissipation structure

    Heat-dissipation design for efficient heat spreading and stable operation

  • Multiple communication interfaces

    Control and implementation of wired, high-speed and standard serial interfaces

  • Signal control and logic circuit design

    Multi-channel signal-control circuits with communication channels integrated in programmable logic

  • Real-time system monitoring

    Real-time temperature and voltage-level sensing and monitoring of the operating environment

  • Signal I/O and circuit protection

    Discrete-signal I/O control and protection circuits against over-voltage and signal interference

Guidance Data Receiver (Weapon Datalink Modem)

MPSOC- and RFSOC-based signal-processing boards and 1T3R modem platforms that let the round receive target and mission data from the ground or shipboard control station in real time.

Operating Concept

Guidance & Control Unit — Operating Concept

Inside a guided-weapon system the guidance & control unit exchanges power, commands and target data with the forward and aft subsystems, controlling the round through every phase of flight. The diagram magnifies the position of the unit within the round and shows the signals exchanged with each subsystem.

Guidance Data Receiver
Forward Subsystems
Nose Cap
  • Incoming signalNose-cap separation signal
  • Incoming signalPower, target data, commands
  • Outgoing signalTarget data, track & detection data
Inertial Measurement Unit
  • Outgoing signalAcceleration, angular rate
  • Incoming signalPower, clock
  • Incoming signalPower, commands
  • Outgoing signalTarget data, mission data
Aft Subsystems
  • Two-way signalDrive commands, responses, status
  • Incoming signalPower
  • Outgoing signalGNSS data, status
  • Incoming signalPower, commands
Flight Measurement Unit
  • Incoming signalIn-round data, power
  • Incoming signalDetonation signal, delay data
  • Outgoing signalStatus data
Guided-rocket configuration — the marked band is where the guidance & control unit sits

Guided-rocket configuration — the marked band is where the guidance data receiver sits

L-SA* Modem Board

In production

L-SA* modem platform development

  • Modem platform development

    Modem-board system platform for high-performance communication

  • High-performance signal-processing design

    Integrated digital and RF signal-processing board built on a multi-function processor

  • RF transceiver architecture

    Multi-channel RF transmit/receive architecture

  • Commercial results and production

    System development completed and series production established

Short-Range Air-to-Air Modem Board

In development

Short-range air-to-air modem platform development

  • Airborne communication modem platform

    Modem-board system dedicated to short-range air-to-air communication

  • High-performance RF signal-processing board

    Domestically developed signal-processing board integrating RF and digital processing

  • Multi-channel RF transceiver architecture

    Multi-channel RF transmit/receive architecture

  • Development status

    Localisation and core-technology development in progress

Ship-** Ⅱ Modem Board

In development

Ship-** Ⅱ modem and weapon-datalink platform development

  • Guided-weapon modem platform

    Modem-board system platform for the next-generation surface-to-air guided-weapon system (Ham**-Ⅱ)

  • High-performance signal-processing design

    Integrated digital and RF signal-processing board built on a multi-function processor

  • Multi-channel RF transceiver architecture

    Multi-channel RF transmit/receive architecture for stable data transfer

  • Development status

    Core technologies implemented; development in progress

L-SA*-Ⅱ Modem Board

In development

L-SA*-Ⅱ modem and weapon-datalink platform development

  • Guided-weapon modem platform

    Modem-board system platform for the next-generation long-range surface-to-air guided-weapon system (L-SA*-Ⅱ)

  • High-performance signal-processing design

    Integrated digital and RF signal-processing board built on a multi-function processor

  • Multi-channel RF transceiver architecture

    Multi-channel RF transmit/receive architecture for stable data transfer

  • Development status

    Core technologies implemented; development in progress

MSA*-Block-Ⅲ Modem Board

In development

MSA*-Block-Ⅲ modem platform development

  • Guided-weapon modem platform

    Modem-board system platform for the next-generation medium-range surface-to-air guided-weapon system (MSA*-Block-Ⅲ)

  • High-performance signal-processing design

    Integrated digital and RF signal-processing board built on a multi-function processor

  • Dual-band RF transceiver architecture

    Flexible RF transmit/receive architecture supporting multiple frequency bands and channels

  • Development status

    Core technologies implemented; development in progress

Actuation Unit (Actuator Controller)

The actuation-unit circuit-card assembly: it takes drive commands from the guidance & control unit, generates the drive output for each actuator axis, and measures actuator status.

Operating Concept

Guidance & Control Unit — Operating Concept

Inside a guided-weapon system the guidance & control unit exchanges power, commands and target data with the forward and aft subsystems, controlling the round through every phase of flight. The diagram magnifies the position of the unit within the round and shows the signals exchanged with each subsystem.

Actuation Unit
Forward Subsystems
Nose Cap
  • Incoming signalNose-cap separation signal
  • Incoming signalPower, target data, commands
  • Outgoing signalTarget data, track & detection data
Inertial Measurement Unit
  • Outgoing signalAcceleration, angular rate
  • Incoming signalPower, clock
  • Incoming signalPower, commands
  • Outgoing signalTarget data, mission data
Aft Subsystems
  • Two-way signalDrive commands, responses, status
  • Incoming signalPower
  • Outgoing signalGNSS data, status
  • Incoming signalPower, commands
Flight Measurement Unit
  • Incoming signalIn-round data, power
  • Incoming signalDetonation signal, delay data
  • Outgoing signalStatus data
Guided-rocket configuration — the marked band is where the guidance & control unit sits

Guided-rocket configuration — the marked band is where the actuation unit sits

MSA*-Block-Ⅲ Actuator Controller

01

Actuation-unit circuit-card assembly

  • Integrated actuator control and computation

    Actuator status measurement, real-time control computation and signal generation

  • Multi-axis drive output

    Dedicated drive outputs for multi-axis actuators

  • Inter-module signal interface

    Stable signal connection between circuit cards and peripheral units

  • Stable power supply

    Supply and distribution of the power the controller needs

Anti-Jam GNSS RF Assembly

Operating Concept

Guidance & Control Unit — Operating Concept

Inside a guided-weapon system the guidance & control unit exchanges power, commands and target data with the forward and aft subsystems, controlling the round through every phase of flight. The diagram magnifies the position of the unit within the round and shows the signals exchanged with each subsystem.

Anti-Jam GNSS Unit
Forward Subsystems
Nose Cap
  • Incoming signalNose-cap separation signal
  • Incoming signalPower, target data, commands
  • Outgoing signalTarget data, track & detection data
Inertial Measurement Unit
  • Outgoing signalAcceleration, angular rate
  • Incoming signalPower, clock
  • Incoming signalPower, commands
  • Outgoing signalTarget data, mission data
Aft Subsystems
  • Two-way signalDrive commands, responses, status
  • Incoming signalPower
  • Outgoing signalGNSS data, status
  • Incoming signalPower, commands
Flight Measurement Unit
  • Incoming signalIn-round data, power
  • Incoming signalDetonation signal, delay data
  • Outgoing signalStatus data
Guided-rocket configuration — the marked band is where the guidance & control unit sits

Guided-rocket configuration — the marked band is where the anti-jam gnss unit sits

Common features

GPS receiver able to operate under attack from external jamming systems

  • Low-noise amplifier design
  • Phase-noise minimisation through reference-oscillator design
  • Multi-channel / multi-band implementation and miniaturisation design
  • Frequency up/down conversion and digital signal conversion design
  • Digital-noise suppression through power-rail isolation

L-SA* Anti-Jam GNSS RF Board

01

Shielded board with eight RF connectors and a high-density signal connector

L-SA*-Ⅱ Anti-Jam GNSS RF Board

02

Next-generation RF board built on the L-SA* RF-board platform

Long-Range Air-to-Ground GNSS RF Board

03

Housing-integrated RF assembly with side-mounted RF ports

Ship-** Missile Ⅱ GNSS RF Board

04

Compact housing with integral mounting lugs and compartmented shielding

Fuze TDD Signal Processor

The signal processor of the target-detection device (TDD) that determines the point of closest approach and issues the detonation signal — demanding both very high-speed digital signal processing and high-reliability power and monitoring design.

Operating Concept

Guidance & Control Unit — Operating Concept

Inside a guided-weapon system the guidance & control unit exchanges power, commands and target data with the forward and aft subsystems, controlling the round through every phase of flight. The diagram magnifies the position of the unit within the round and shows the signals exchanged with each subsystem.

Forward Subsystems
Nose Cap
  • Incoming signalNose-cap separation signal
  • Incoming signalPower, target data, commands
  • Outgoing signalTarget data, track & detection data
Inertial Measurement Unit
  • Outgoing signalAcceleration, angular rate
  • Incoming signalPower, clock
  • Incoming signalPower, commands
  • Outgoing signalTarget data, mission data
Aft Subsystems
  • Two-way signalDrive commands, responses, status
  • Incoming signalPower
  • Outgoing signalGNSS data, status
  • Incoming signalPower, commands
Flight Measurement Unit
  • Incoming signalIn-round data, power
  • Incoming signalDetonation signal, delay data
  • Outgoing signalStatus data
Guided-rocket configuration — the marked band is where the guidance & control unit sits

Guided-rocket configuration — the marked band is where the fuze sits

Ship-** Ⅱ Fuze TDD Signal Processor

01
  • Ultra-high-speed signal processing and algorithms

    High-performance signal-processing circuits for real-time handling of large data volumes and complex algorithms

  • High-speed data interfaces

    Serial interfaces optimised for fast, stable transfer of large data between the core compute modules

  • Signal integrity and noise control

    Advanced routing and board design that preserve high-speed signal quality and minimise analogue noise

  • High-reliability power management and protection

    Stable power distribution with input-protection circuits that prevent system damage

  • Real-time health monitoring

    Real-time sensing and monitoring of voltage, current and temperature for safe operation

Hae* Fuze TDD Signal Processor

02
  • High-speed RF signal processing and logic

    Logic optimised for real-time computation on RF signals and high-speed digital signal processing

  • High-efficiency power management and conversion

    Miniature, high-efficiency power conversion and noise-filtering circuits for stable communication and control modules

  • High-speed, low-latency internal interfaces

    Real-time, high-speed, low-latency data links between the core control components

  • Real-time health monitoring

    Real-time sensing and remote monitoring of voltage, current, temperature and output status for system reliability

Seeker (Frequency Synthesizer)

Operating Concept

Guidance & Control Unit — Operating Concept

Inside a guided-weapon system the guidance & control unit exchanges power, commands and target data with the forward and aft subsystems, controlling the round through every phase of flight. The diagram magnifies the position of the unit within the round and shows the signals exchanged with each subsystem.

Seeker
Forward Subsystems
Nose Cap
  • Incoming signalNose-cap separation signal
  • Incoming signalPower, target data, commands
  • Outgoing signalTarget data, track & detection data
Inertial Measurement Unit
  • Outgoing signalAcceleration, angular rate
  • Incoming signalPower, clock
  • Incoming signalPower, commands
  • Outgoing signalTarget data, mission data
Aft Subsystems
  • Two-way signalDrive commands, responses, status
  • Incoming signalPower
  • Outgoing signalGNSS data, status
  • Incoming signalPower, commands
Flight Measurement Unit
  • Incoming signalIn-round data, power
  • Incoming signalDetonation signal, delay data
  • Outgoing signalStatus data
Guided-rocket configuration — the marked band is where the guidance & control unit sits

Guided-rocket configuration — the marked band is where the seeker sits

Common features

Frequency signal generator for precision target detection

  • High-resolution design using DDS
  • Vibration-tolerant low-phase-noise design
  • LFM and HRR waveform generation design
  • High-speed switching design
  • Ku-band RF signal generation design

Cheon*-Ⅰ Frequency Synthesizer

01

Single shielded housing with three RF connectors

Cheon*-Ⅱ Frequency Synthesizer

02

Housing with multiple shielded cavities

Hae* Frequency Synthesizer

03

Two-unit set: reference signal generator and synthesizer body

L-SA* Frequency Synthesizer

04

Multi-cavity shielded structure with side-mounted RF ports

Seeker (Servo Controller)

Servo controllers that stabilise the line of sight of imaging seekers.

L-SA*-Ⅱ Imaging Seeker Servo Controller

01

Servo-control circuit-card assembly driving the imaging-seeker gimbal

  • BiSS-C/SSI encoder interface design
  • RS-422/RS-232 communication interface design
  • PMSM servo-motor current control
  • Isolated phase-current feedback circuit design
  • Isolation circuit design between the control and drive stages
  • Temperature and voltage-level monitoring interface design
  • Discrete-signal I/O and protection circuit design

Weapon Employment Support Equipment · Aerial Target Drone

Cockpit and portable equipment that supports weapon employment, together with the guidance & control unit of an aerial target drone: the command & communication device that transmits the mission to an air-launched guided munition from the cockpit, the code loader that loads and transfers crypto codes, and the GCU of the supersonic cruise target drone used in air-defence live-fire training.

Employment concept of the air-launched guided munition
Operating concept of the command & communication device
Module configuration of the command & communication device
IFF architecture
Employment concept of the code loader

Command & Communication Device — Air-Launched Guided Munition (Domestic / Export)

In production

Host aircraft: F-5E/F, F-15K, F-4E, (K)F-16C/D, FA-50

  • Real-time computation and display of the release area from aircraft latitude, longitude, altitude and speed
  • Optimised map rendering
  • Day and night GUI skins, with four-step LCD backlight control for night operation
  • One-touch mission erase for pilot safety in an emergency
  • Compliant with the defence map-symbol standard MND-STD-0023A-02
  • Compliant with DAPA weapon-system software development and management regulations

OOO Code Loader — OO System OOOO Upgrade

02
  • Performs code-loader and code-transfer functions, with OOOO operating-concept setting
  • Consolidates the separate code-entry and code-transfer accessories into a single device
  • FPGA-linked protocol design for sharing codes between code loaders
  • Security design that erases the codes automatically on disassembly or battery depletion

Supersonic Cruise Aerial Target Drone GCU (Domestic / Export)

03
  • Power management and drive control

    Stable multi-channel power supply with built-in BLDC motor drive and Hall-sensor input circuits

  • High-performance processing and system control

    DSP- and FPGA-based processing for communication with, and integrated control of, the internal components

  • Signal processing and I/O control

    Multi-channel I/O control, constant-current control outputs, analogue signal processing and protection circuits

  • Communication and interfaces

    Multi-channel communication interfaces across serial, Ethernet and other standards

  • Real-time system monitoring

    Real-time temperature and voltage-level monitoring for a stable operating environment