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Section V.  SYSTEMS SIMULATED
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TM-55-6930-212-10 Pyrometer and Thermocouple Tester Field Type N-3A Manual
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CHAPTER 3 AVIONICS

TM 55-6930-212-10 2-83.  VIBRATION SIMULATION. 2-84.  An electrohydraulic seat shaker transmits vibrational effects to the trainees, but its effects are isolated from other compartment-mounted hardware and other simulator occupants. 2-85.  COCKPIT INSTRUMENTATION SIMULATION  . 2-86.  All cockpit instruments and controls are modified actual aircraft instruments that accept outputs from dc analog circuitry under computer control and respond with the desired deflections or rotations.  Three basic types of circuitry are used to drive the following classes of instruments: Meter movement instruments Servo instruments Synchro instruments 2-87.  RADIO COMMUNICATION AND INTERCOMMUNICATION SYSTEM SIMULATION. 2-88.  An internal communication system (ICS) under computer control directs audio signals by means of C-6533/ARC control panels for: Trainee to trainee IOS to observer Trainee to IOS Trainee to observer IOS to trainee IOS to computer room Observer to IOS Computer room to IOS NOTE The simulator C-6533 ICS operates identically to that in the helicopter.  The observer station ICS  control  box  switches  must  be  in  the  following  positions  for  the  instructor  to  observe communication: (1) all toggle switches down/OFF; and (2) selector switch on position 5. The  IOS  C-6533  ICS  control  box  switches  must  be  in  the  following  positions  for  total  IOS communication functions: (1) toggle switches 1 through 5 up/ON; (2) AUX and NAV switches down/OFF; and (3) selector switch on position 5. 2-89.  MALFUNCTION SIMULATION. 2-90.  Approximately 220 malfunctions can be inserted by the instructor.  Malfunctions are realistic, and they provide the pilot and copilot with meaningful training in emergency responses. 2-91.  CONTROL LOADING. 2-92.    The  control  loading  system  provides  a  realistic  and  responsive  feel  to  the  simulated  helicopter  flight  controls. Electrohydraulic   units,   combined   with   a   mechanical   linkage   system,   produce   initiating   and   reactive   forces   for   the controls.  Simulation computer feedback causes the appropriate motions of the aircraft in flight.  During a demonstration playback,  the  cockpit  flight  controls  are  driven  by  the  computer  and  appropriately  positioned  in  response  to  aircraft motion. 2-17/(2-18 blank)

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