packageAircraftRequirements
Library of examples to demonstrate requirement definitions for aircrafts
Extends from Modelica.Icons.ExamplesPackage (Icon for packages containing runnable examples).
Information
This 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.
Contents
| 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 |