Elite Simulation S623T, Руководство оператора, Страница: 53 / 141

5.3 Aircraft Systems Simulation
5.3.1 Electrical System
Changing the status of electrical consumers in the cockpit (e. g. switching on / off Avionics panel) is
refl ected in the consumption of electricity. Should the helicopter’s electrical systems run on battery
only without being constantly fed by the generator, battery load will decrease.
5.3.2 Engine System
The engine and the associated controls and indicators are simulated as described in the he-
licopter data. The basis for the turbine and helicopter model is a Eurocopter AS355F1 Twin
Squirrel.
Simulation of the power plant includes turbines start on the ground and in the air, normal gov-
erned operation, acceleration, deceleration and shut down. Variations of the effects of altitude,
airspeed and ambient temperature are included in the performance computations.
Characteristics for the applicable turbines and their effect on the fl ight path are reproduced in re-
sponse to engine control selections.
The turbines monitoring system has the capability of depicting a realistic representation of turbine
operations.
Rotor control and operation are realistically simulated.
Engine sound is realistically modeled during start- and continuous operation.
5.3.3 Fuel System
The Aircraft fuel system is simulated in accordance with helicopter data. The effect of fuel deple-
tion is simulated. Fuel quantity indicators are simulated from helicopter data.
5.3.4 Steering
The normal system controls, indicators and warning sounds are simulated according to the heli-
copter data.
5.3.5 Flight Control System
The fl ight controls are installed for a single or dual pilot / single or dual cyclic operation in the cock-
pit and functions according to the available helicopter data. A Dynamic Control Load System (DCL)
is installed.