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MOTION SYSTEM
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TM-55-6930-212-10 Pyrometer and Thermocouple Tester Field Type N-3A Manual
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Section II.  INSTRUCTOR OPERATOR STATION DESCRIPTION

TM 55-6930-212-10 introduced by the instructor produce the appropriate motion effects of yaw and roll, climb or descent, and variations in airspeed.  Superimposed upon the background motion, the motion system provides characteristic periodic oscillations of the aircraft, lateral instability, and aircraft vibrations up to 5 cycles per second.  In addition, continuous higher-frequency vibrations  are  simulated  using  a  seat  shaker  in  lieu  of  the  motion  system.    Effects  of  sling  load  oscillations  are  also simulated through the motion system. 2-25.  ABNORMAL FLIGHT. 2-26.  The  motion  system  reproduces  the  effects  of  rotor  out-of-track  and  rotor  out-of-balance  failures.    The  motion simulated  includes  the  effect  of  momentary  incorrect  control  inputs.    Hydraulic  failure  resulting  in  abnormal  control configurations results in appropriate motion cues.  High-speed characteristics and trim changes also cause appropriate effects in the motion system. 2-27.  VISUAL SYSTEM. 2-28.  The pilot/copilot stations have forward, left, and right side windows, and chin window visual displays.  The visual generation system provides imagery to every sensor display in the simulator, including the out-the-window (OTW) scene. 2-29.  DIGITAL IMAGE GENERATOR. 2-30.  The  digital  image  generator  (DIG)  system  is  a  full-color  visual  display  that  provides  imagery  for  day,  dusk,  and night scenes.  The DIG is used for the six out the-window displays (two front, two side, and two chin window).  It also provides imagery that represents night vision goggles (NVG) displays and simulates the action of a searchlight on the visual displays. 2-31.  The two chin window displays are high-resolution, full-color visual displays.  One display serves as the pilot's chin window, and the other serves as the copilot's chin window.  Video signals are sent to each chin window display monitor from the DIG via distribution amplifiers in the visual interface cabinet. 2-32.  The fields-of-view (FOV) for the windows are as follows: Window Pilot Copilot Front Up 13.3 (±0.5)° Up 13.3 (±0.5)° and Down 22.7 (±0.5)° Down 22.7 (±0.5)° side Right 24 (±0.5)° Right 24 (±0.5)° Left 24 (±0.5)° Left 24 (±0.5)° Chin Horizontal 22 (-0.5, +3)° Horizontal 22 (-0.5.+3)° Vertical 30 (-0.5, +3)° Vertical 30 (-0.5, +3)° Centered 40 (±0.5)° down, 27.5 (+0.5)° left and right (both) 2-33.  COMPUTER SYSTEM. 2-34.  The  simulator  consists  of  the  main  computational  system  (MCS),  which  is  made  up  of  central  processing  units (CPU's  1,  2,  and  3)  and  their  associated  auxiliary  processing  units  (APU's).    Each  CPU  has  memory  that  can  be accessed only by it and its associated APU's. 2-6

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