TM 55-6930-214-10
2-29. COCKPIT INSTRUMENTATION SIMULATION. All cockpit instruments and controls
simulated are actual modified aircraft instruments. They 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
2-30. RADIO COMMUNICATION AND INTERCOMMUNICATION SYSTEM (ICS) SIMULATION. The
radio communications, guidance, and ICS systems simulated are listed and described
in Chapter 3.
2-31. MALFUNCTION SIMULATION. There are 336 insertable, simulated malfunctions
a v a i l a b l e . These malfunctions are divided into five systems: flight, circuit
breakers, communications, tactics, and navigation. (Refer to tables 7-15 and 7-16
for listing and descriptions).
2-32. CONTROL LOADING. The control loading system provides a realistic and re-
sponsive feel to the simulated helicopter flight controls. Electrohydraulic units
combined with a mechanical linkage system produce control initiating and reactive
forces. Feedback from the simulation computer results in appropriate motions of
the aircraft in flight. During a demonstration playback, the cockpit flight con-
trols are driven by the computer and appropriately positioned in response to the
motion of the aircraft.
WARNING
Flight controls may move abruptly upon system turn-on, initial
conditions insertion, demonstration maneuvers or conditions store/
reset. Keep clear of controls until neutral position is reached.
Simulation for the following armament systems is provided:
2-33.
ARMAMENT SYSTEMS.
M-230E1 30-mm area weapon system
HELLFIRE missile system
M-261 19-tube FFAR rocket launcher
Integrated helmet and display sight system (IHADSS)
Pilot night vision system (PNVS)
Optical relay tube (ORT)
Target acquisition and designation system (TADS)
Laser rangefinder/designator
Laser tracker
Video display unit (VDU)
Video recorder system (VRS)
2-31/(2-32 blank)
Change
