Modular Control Electronics Unit



Based on heritage Moog controllers, the robust architecture of the Control Electronics Unit (CEU) is derived from flight hardware designs with common solutions for multiple applications. 

 

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Overview:

Existing three-card or five-card slot enclosures can be used to accommodate and provide the following controller applications:

  • Electromechanical (EM) Actuation
  • Electrohydraulic (EH) Actuation
  • Electrohydrostatic (EHA) Actuation
  • Communication Converter
  • Electric Power Subsystem Control
  • Hydraulic Power Subsystem Control
  • Power Distribution
  • Battery Management Control 
  • Main Engine Fluid Control 
  • Propellant Management System Control 
  • Roll Control System

The CEU is also extensible to the following with new circuit card assemblies (CCAs):

  • Flight Computer
  • Data Acquisition Package
  • Stage Interface Unit
  • Solid Motor Ignition

Logic Processing Unit Card

  • Large FPGA for logic implementation
  • 4 LVDT/RVDT/Resolver Interfaces
  • RS-422 Comm. Interface 

Fluid Sensors and Controls Interface Card

  • 16 Pressure Sensor Interfaces
  • 8 Temperature Sensor Interface
  • 2 Solenoid Drivers
  • 2 Servovalve Drivers

Communication Card

  • 4 RS-422 Comm. Interfaces
  • 2 Analog Comm. Interface
  • Telemetry Only RS-422
  • 3 Cross Channel Data Links
  • 1 MIL-STD-1553B Redundant Comm. Interface
  • 16 Generic Digital Inputs
  • 8 Generic Digital Outputs
  • EEPROM for servo-gain storage and other uses

Low Voltage Power Supply

  •  Filtered 28V Out
  • Array of Low Level Voltages to Support other CCAs
  • Isolated Voltages as needed to support grounding needs

Power Stage Interface Card

  • 2 Channels of 3-phase motor bridge gate drivers
  • 2 Channels of 3-phase motor current sense interface
  • Bus voltage and current sense interface
  • Power Stage Built-in-Test Interface

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