.Modelica_Requirements.Examples.AircraftRequirements

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