Zynq SoC-Based High-Speed Digital Servo Controller
High-speed Zynq SoC-based servo controller integrating digital closed-loop control with a high-power MOSFET motor-drive stage for single-EMA actuation.
All Systems & Applications
Missile Guidance & Navigation Systems
Control, actuation and mission-electronics solutions supporting guidance, navigation and flight-control architectures for advanced missile systems.
Overview
RTS develops flight-control, actuation and mission-electronics subsystems for missile and flight-vehicle programmes, integrating servo control, embedded processing, power electronics and precision electromechanical engineering into compact, application-specific solutions.
The portfolio spans high-speed digital servo controllers, single-, dual- and quad-channel EMA control, high-power actuation electronics, solenoid-valve sequencing, fuel-flow control, wing-control electronics, precision locking mechanisms and linear actuators. RTS experience covers actuation classes from compact 0.3-ton wing-control systems to high-load 8-ton EMA applications, with several developed systems progressing through flight testing and programme-level validation.
Systems Developed for Demanding Applications
Zynq SoC-Based High-Speed Digital Servo Controller
Developed for high-speed electromechanical actuation, this controller combines Zynq SoC processing, digital closed-loop servo control and a high-power motor-drive inverter within a compact architecture. The controller is intended for flight-control applications requiring fast response, precise actuator positioning and tightly integrated embedded processing and power electronics.
Key Features
Zynq SoC-based digital-control architecture
Closed-loop single-EMA servo control
Integrated high-power motor-drive inverter
MOSFET-based power amplification
Technical Overview
Processor
Zynq SoC
Configuration
Single EMA controller
Power Stage
MOSFET based
Electrical Class
150 V / up to 160 A
High-Power Dual-Channel IGBT Servo Controller
Dual-channel digital servo controller for 8-ton-class EMA actuation, combining closed-loop position control with a high-current IGBT power stage.
High-Power Dual-Channel IGBT Servo Controller
This high-power dual-channel servo controller was developed for large electromechanical actuator loads. It combines microcontroller-based digital control with dual actuation channels and IGBT power amplification to deliver closed-loop position control under demanding load conditions. The architecture is suited to applications requiring high actuator force, controlled slew rate and reliable high-power operation.
Key Features
Dual-channel digital servo-control architecture
8-ton-class electromechanical actuator control
IGBT-based high-power amplification
Closed-loop position control under high load
Technical Overview
EMA Load Class
8-ton class
Configuration
Dual channel
Full-Load Slew Rate
15°/s
Electrical Class
150 V / up to 400 A
Digital Servo Controller for High-Load EMA Systems
Dual-channel digital servo controller developed for an 8-ton EMA system, with high-power MOSFET drive electronics and precise closed-loop actuation control.
Digital Servo Controller for High-Load EMA Systems
Designed for high-load electromechanical actuation, this controller integrates dual-channel digital control, embedded processing and high-power motor-drive electronics. It supports precise closed-loop positioning of large actuators and is engineered around the electrical and dynamic requirements of heavy flight-control actuation systems.
Key Features
Dual-channel digital controller architecture
8-ton EMA system class
Integrated high-power MOSFET motor-drive stage
Closed-loop control for large actuator loads
Technical Overview
EMA System Class
8-ton
Configuration
Dual channel
Validated Slew Rate
7°/s at 6-ton load
Electrical Class
100 V / up to 300 A
Quad-Channel Digital Servo Controller
ADSP-based four-channel servo controller for coordinated closed-loop control of 1-ton-class EMA systems across multiple aerodynamic-control axes.
Quad-Channel Digital Servo Controller
This quad-channel digital servo controller is designed for coordinated control of multiple electromechanical actuators. An ADSP-based processing architecture executes the control functions while four servo channels manage actuator positioning for aerodynamic manoeuvring. The system combines multi-axis control, feedback processing and MOSFET-based power amplification within a single controller architecture.
Key Features
ADSP-based embedded processing
Four independent servo-control channels
1-ton-class EMA control
MOSFET-based power amplification
Technical Overview
EMA Load Class
1-ton class
Channels
4
Processor
ADSP based
Electrical Class
100 V / 100 A
Multi-Channel Quick Response Solenoid Valve Controller
Twenty-channel quick-response controller for coordinated operation of up to 40 solenoid valves with redundant communication and high-current switching.
Multi-Channel Quick Response Solenoid Valve Controller
Developed for applications requiring rapid and coordinated valve actuation, this controller manages 20 control channels and the functional operation of up to 40 solenoid valves. The architecture combines embedded sequencing, high-current MOSFET switching and dual-redundant MIL-STD-1553 communication for integration with onboard command systems.
Key Features
20-channel control architecture
Control of up to 40 solenoid valves
Dual-redundant MIL-STD-1553 communication
MOSFET-based high-current switching
Technical Overview
Controller Channels
20
Valve Control
Up to 40 solenoid valves
Communication
Dual-redundant MIL-STD-1553
Electrical Class
50 V / up to 140 A
Electronic Fuel Flow Controller
Zynq SoC-based digital controller for closed-loop fuel-flow regulation through electromagnetic-valve control, signal conditioning and MOSFET power electronics.
Electronic Fuel Flow Controller
The Electronic Fuel Flow Controller combines Zynq SoC-based digital processing, signal conditioning and electromagnetic-valve control to regulate fuel mass flow in a closed-loop process. The controller translates control commands into precise valve operation while supporting the feedback and conditioning functions required for adaptive fuel-flow regulation.
Key Features
Zynq SoC-based digital controller
Closed-loop fuel-flow regulation
Integrated signal conditioning
Electromagnetic-valve control with MOSFET power stage
Technical Overview
Processor
Zynq SoC
Operating Voltage
28 V
Control
Closed-loop fuel-flow control
Power Stage
MOSFET based
Wing Servo Controller Unit
Compact servo controller for a 0.3-ton EMA wing mechanism, integrating analog control electronics with a MOSFET motor-drive inverter.
Wing Servo Controller Unit
The Wing Servo Controller Unit integrates servo-control electronics with a motor-drive inverter to operate an electromechanical wing mechanism. It supports controlled deployment and positioning through a compact architecture combining analog control functions, motor-drive electronics and MOSFET-based power amplification.
Key Features
0.3-ton EMA wing-control application
Integrated servo controller and motor-drive inverter
Controlled wing deployment and positioning
MOSFET-based power amplification
Technical Overview
EMA Load Class
0.3-ton
Operating Voltage
28 V
Current Class
10 A
Power Stage
MOSFET based
Fin Locking Mechanism
Solenoid-operated precision mechanism for locking aerodynamic-control surfaces during carriage and releasing them during deployment.
Fin Locking Mechanism
The Fin Locking Mechanism is a precision electromechanical assembly designed to hold aerodynamic-control surfaces securely during carriage and release them when deployment is required. The mechanism combines a solenoid-operated locking concept with precision-machined structural elements designed to withstand aerodynamic loading while maintaining repeatable release behaviour.
Key Features
Solenoid-operated lock-and-release mechanism
Designed for aerodynamic-control surfaces
Precision-machined structural assembly
Compact short-duration actuation
Technical Overview
Operating Voltage
28 V
Maximum Power
280 W
Operating Window
Up to 200 ms
Function
Fin lock & release
3000N Linear Actuator
Compact PM-BLDC linear actuator delivering 3000N-class force through a ball-screw drive for high-precision electromechanical positioning.
3000N Linear Actuator
RTS developed the 3000N Linear Actuator as a compact electromechanical actuation solution for demanding aerospace applications. The design combines a PM-BLDC motor with ball-screw transmission to deliver high linear force, controlled stroke and repeatable motion while meeting tight packaging and mechanical-integration requirements.
Key Features
PM-BLDC motor-driven linear actuation
Ball-screw rotary-to-linear conversion
High-force compact actuator architecture
Designed for precision electromechanical positioning
Technical Overview
Stall Force
3200 N
Stroke
0–75 mm
Linear Speed
52 mm/s
Electrical
28 V / 15 A