Constraints. More...
#include <CPACSPointPerformanceConstraints.h>
Protected Attributes | |
boost::optional< CPACSDoubleConstraintBase > | m_acceleration |
Rate of velocity [m/s^2]. More... | |
boost::optional< CPACSDoubleConstraintBase > | m_altitude |
Constant altitude [m]. More... | |
boost::optional< CPACSDoubleConstraintBase > | m_angleOfAttack |
Angle of attack [deg]. More... | |
boost::optional< CPACSDoubleConstraintBase > | m_calibratedAirSpeed |
Calibrated airspeed [m/s]. More... | |
boost::optional< CPACSDoubleConstraintBase > | m_climbAngle |
Climb angle [deg]. More... | |
boost::optional< CPACSDoubleConstraintBase > | m_duration |
Duration [s]. More... | |
boost::optional< CPACSDoubleConstraintBase > | m_machNumber |
Mach number [-]. More... | |
CPACSPointPerformanceDefinition * | m_parent |
boost::optional< CPACSDoubleConstraintBase > | m_rateOfClimb |
Rate of climb [m/s]. More... | |
boost::optional< CPACSDoubleConstraintBase > | m_rateOfTurn |
Rate of turn [deg/s]. More... | |
boost::optional< CPACSDoubleConstraintBase > | m_thrustSetting |
Thrust setting for derated engine as fraction of max. thrust (e.g.: for powered descents, deceleration not at IDLE, manoevres) More... | |
Private Member Functions | |
CPACSPointPerformanceConstraints (const CPACSPointPerformanceConstraints &)=delete | |
CPACSPointPerformanceConstraints (CPACSPointPerformanceConstraints &&)=delete | |
CPACSPointPerformanceConstraints & | operator= (const CPACSPointPerformanceConstraints &)=delete |
CPACSPointPerformanceConstraints & | operator= (CPACSPointPerformanceConstraints &&)=delete |
Constraints.
Constraint settings for the point performance definition
TIGL_EXPORT tigl::generated::CPACSPointPerformanceConstraints::CPACSPointPerformanceConstraints | ( | CPACSPointPerformanceDefinition * | parent | ) |
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TIGL_EXPORT CPACSPointPerformanceDefinition* tigl::generated::CPACSPointPerformanceConstraints::GetParent | ( | ) |
TIGL_EXPORT const CPACSPointPerformanceDefinition* tigl::generated::CPACSPointPerformanceConstraints::GetParent | ( | ) | const |
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Rate of velocity [m/s^2].
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Constant altitude [m].
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Angle of attack [deg].
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Calibrated airspeed [m/s].
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Climb angle [deg].
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Duration [s].
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Mach number [-].
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Rate of climb [m/s].
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Rate of turn [deg/s].
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Thrust setting for derated engine as fraction of max. thrust (e.g.: for powered descents, deceleration not at IDLE, manoevres)