Smart Display Unit-I

Smart Display Unit-I

Smart Display Unit-I works as a centralized monitoring and control unit of the navigation and mission avionics of the fighter aircraft. SDU-I performs the functions of a display computer and performs these tasks through the use of 1553B bus and discrete I/Os. SDU-I receives data from the Line Replaceable Units (LRUs) of the avionics system via the 1553B bus and discrete signal interfaces.

OVERVIEW

  • Avionics management
  • Integrates aircraft’s subsystems and sensors
  • Provide centralized control and display of avionics functions such as communications, navigation and mission management.

Block Diagram

SPECIFICATIONS

6 different Replaceable Modules (connected on the VME32 backplane):

  • CPU Module
  • MBI (Mux Bus Interface)
  • Discrete Interface Module (DIM)
  • Key panel assembly
  • Display assembly
  • Power Supply Module
Electrical Characteristics:
28 V DC (15 to 33.5 V) 40 W max
Integral lighting: 0 to 5 V AC RMS / 400 Hz 10 W max
Physical characteristics:
Width 5.00 in. (127.0 ± 0.2 mm)
Height 7.11 in (180.6 mm max.)
Depth 6.75 in (171.5 mm max.)
Standards:
  • MIL-STD 810 E including MIL-STD-2164 (Avionics ESS)
  • MIL-P-55110 E
  • MIL-STD 454 G 30 April, 1984
  • MIL-E-5400T
  • MIL-STD 1760C
  • MIL-STD-461D

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