.Modelica_Requirements.Examples.AircraftRequirements .Modelica_Requirements.Examples.AircraftRequirementsThis package contains example models to demonstrate how typical requirements appearing in aircraft design can be formulated with the Modelica_Requirements library. These examples have been provided by the aircraft manufacturer Dassault Aviation.
| Name | Description |
|---|---|
 LimitedControlFrequency | Requirement: The frequency of the control signal is limited |
 MinimumAirDistributionPerformance | Requirement: If only one engine is running, the air distribution circuit shall provide nominal performance |
 MinimumOperationalServiceLife | Requirement: The aircraft shall be designed for a minimum operational service life. |
 MaximumCabinTemperatureIncrease | Requirement: The temperature increase of the cabin area is limited to ensure passenger comfort |
 MaximumCabinDissipatedPowerIncrease | Requirement: The dissipated power of cabin area is limited to ensure passenger comfort |
 LimitedCabinAltitudeRateOfChange | Requirement: The cabin altitude rate of change is limited by the pressure bump duration domain to ensure passenger comfort |
 LimitedFreshECSFlow | Requirement: The fresh airflow entering the pressurized areas shall be within the given domain |
 PreventHeatExchangerClogging | Requirement: Cold heat exchanger clogging shall not occur |
 TriggerAPUStartSequence | Requirement: The Auxiliary Power Unit shall be started after successive start failures of one of the engines |