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| | DtAirspeedCalculator () |
| | Default constructor; assumes a maximum population of 100 samples. More...
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| | DtAirspeedCalculator (const DtAirspeedCalculator &orig) |
| | copy constructor More...
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| virtual | ~DtAirspeedCalculator () |
| | destructor More...
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| const DtAirspeedCalculator & | operator= (const DtAirspeedCalculator &orig) |
| | assignment operator More...
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| virtual void | convertSpeedtoAllAirSpeeds (const DtVrfObjectStateRepository *stateRep, double &groundSpeed, double &trueAirSpeed, double &indicatedAirSpeed, double &machSpeed, double currentAlt, DtAirSpeedType currentSpeedType) |
| | Convert a speed with an Air Type into all air Speed types taking into account entity location and environment state at that location. More...
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| virtual double | tasFromGroundSpeed (const double groundSpeed, const double heading, const double windSpeed, const double windDirection) const |
| | true air speed from ground speed in meters per second groundSpeed and windSpeed is meters per second heading and windDirection are radians More...
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| virtual double | iasFromTas (const double trueAirspeed, const double altitude) const |
| | indicated air speed from true air speed in meters per second This implementation uses the 2% loss per 305m of altitude rule of thumb. More...
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| virtual double | machFromTas (const double trueAirspeed, const double temperature, const double pressure) const |
| | mach from true air speed trueAirspeed is meters per second temperature is in Celcius pressure is in kPa More...
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| virtual double | machFromTas (const double trueAirspeed, const double temperature, const double pressure, const double altitude) const |
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| virtual double | groundSpeedFromTas (const double tas, const double heading, const double windSpeed, const double windDirection) const |
| | ground speed from true air speed in meters per second groundSpeed and windSpeed is meters per second heading and windDirection are radians More...
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| virtual double | tasFromIas (const double indicatedAirspeed, const double altitude) const |
| | true air speed from indicated air speed in meters per second This implementation uses the 2% loss per 305m of altitude rule of thumb. More...
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| virtual double | tasFromMach (const double trueAirspeed, const double temperature, const double pressure) const |
| | true air speed from mach trueAirspeed is meters per second temperature is in Celcius pressure is in kPa More...
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| virtual double | tasFromMach (const double trueAirspeed, const double temperature, const double pressure, const double altitude) const |
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class DtAirspeedCalculator:
DtAirspeedCalculator provides an interface for calculating true air speed, indicated air speed and mach.