A stage represents one stage in the vehicle. More...

#include <WsfTBM_Mover.hpp>

Public Member Functions
	Stage ()
bool	Initialize (double aStageStartTime)
bool	Initialize2 ()
bool	ProcessInput (UtInput &aInput)
double	RemainingInitialMass () const
	The sum of the initial masses of this and the subsequent stages (kg).
double	RemainingBurnoutMass () const
	The sum of the empty (burnout) mass of this and the initial masses of the subsequent stages (kg).

Input values
double	mBallisticCoeff
	Beta (N/m^2).
double	mEmptyMass
double	mFuelMass
double	mFuelMassFraction
double	mTotalMass
double	mThrust
	The thrust (N).
double	mSpecificImpulse
	The specific impulse (sec).
double	mThrustDuration
	The engine burn time (sec).
double	mPreIgnitionCoastTime
double	mPreSeparationCoastTime
double	mCd0
	Zero-lift drag coefficient (C_d0).
double	mReferenceArea
	Reference area.

Derived values
double	mWdot
	The time-rate-of-change of the vehicles weight (NOT MASS) while the engine of this stage is burning.
double	mPayloadMass
double	mS_Cd0
	The surface area times the drag coefficient (m^2).
double	mInitialTime
	The time relative to launch and state when the stage comes into existence (previous stage separates).
double	mInitialState [9]
double	mIgnitionTime
	The time relative to launch and state when the engine ignites.
double	mIgnitionState [9]
double	mBurnOutTime
	The time relative to launch and state when the engine burns out.
double	mBurnOutState [9]
double	mSeparationTime
	The time relative to launch when the stage separates from the vehicle.

Detailed Description

A stage represents one stage in the vehicle.

Constructor & Destructor Documentation

◆ Stage()

WsfTBM_Mover::Stage::Stage ( )

Member Function Documentation

◆ Initialize()

bool WsfTBM_Mover::Stage::Initialize ( double aInitialTime )

Validate and initialize a stage.

Returns: 'true' if successful, 'false' if unsuccessful.

Compute thrust data.

References mBurnOutTime, mEmptyMass, mFuelMass, mFuelMassFraction, mIgnitionTime, mInitialTime, mPreIgnitionCoastTime, mPreSeparationCoastTime, mSeparationTime, mSpecificImpulse, mThrust, mThrustDuration, mTotalMass, mWdot, and ok.

◆ Initialize2()

bool WsfTBM_Mover::Stage::Initialize2 ( )

Perform second pass initialization of a stage.

Returns: 'true' if successful, 'false' if unsuccessful.

References mBallisticCoeff, mCd0, mReferenceArea, mS_Cd0, and RemainingBurnoutMass().

Referenced by WsfTBM_Mover::Initialize().

◆ ProcessInput()

bool WsfTBM_Mover::Stage::ProcessInput ( UtInput & aInput )

Process potential inputs for a stage.

Parameters

aInput The input stream.

Returns: 'true' if the command was a stage related command or 'false' if not.

References mBallisticCoeff, mCd0, mEmptyMass, mFuelMass, mFuelMassFraction, mPreIgnitionCoastTime, mPreSeparationCoastTime, mReferenceArea, mSpecificImpulse, mThrust, mThrustDuration, and mTotalMass.

◆ RemainingBurnoutMass()

double WsfTBM_Mover::Stage::RemainingBurnoutMass ( ) const

inline

The sum of the empty (burnout) mass of this and the initial masses of the subsequent stages (kg).

References mEmptyMass, and mPayloadMass.

Referenced by WsfTBM_Mover::Initialize2(), and Initialize2().

◆ RemainingInitialMass()

double WsfTBM_Mover::Stage::RemainingInitialMass ( ) const

inline

The sum of the initial masses of this and the subsequent stages (kg).

References mEmptyMass, mFuelMass, and mPayloadMass.

Referenced by WsfTBM_Mover::Initialize2().

Member Data Documentation

◆ mBallisticCoeff

double WsfTBM_Mover::Stage::mBallisticCoeff

Beta (N/m^2).

The ballistic coefficient (N/m^2)

Note: This should be the coefficient for the composite vehicle consisting of this and all subsequent stages.

Referenced by WsfTBM_Mover::Initialize2(), Initialize2(), ProcessInput(), and Stage().

◆ mBurnOutState

double WsfTBM_Mover::Stage::mBurnOutState[9]

Referenced by WsfTBM_Mover::ComputeTransitionStateVectors(), WsfTBM_Mover::Initialize2(), and Stage().

◆ mBurnOutTime

double WsfTBM_Mover::Stage::mBurnOutTime

The time relative to launch and state when the engine burns out.

Referenced by WsfTBM_Mover::ComputeTransitionStateVectors(), Initialize(), WsfTBM_Mover::Initialize2(), WsfTBM_Mover::ScheduleScriptEvents(), and Stage().

◆ mCd0

double WsfTBM_Mover::Stage::mCd0

Zero-lift drag coefficient (C_d0).

Referenced by Initialize2(), ProcessInput(), and Stage().

◆ mEmptyMass

double WsfTBM_Mover::Stage::mEmptyMass

Mass of the THIS stage minus the mass of the fuel on THIS.

Note: This does NOT include the mass of the subsequent stages.

Referenced by Initialize(), WsfTBM_Mover::Initialize2(), ProcessInput(), RemainingBurnoutMass(), RemainingInitialMass(), and Stage().

◆ mFuelMass

double WsfTBM_Mover::Stage::mFuelMass

Mass of just the fuel on THIS stage.

Note: This does NOT include the mass of the subsequent stages.

Referenced by Initialize(), WsfTBM_Mover::Initialize2(), ProcessInput(), RemainingInitialMass(), and Stage().

◆ mFuelMassFraction

double WsfTBM_Mover::Stage::mFuelMassFraction

The fraction of the total mass of THIS stage that is fuel.

Note: This does NOT include the mass of the subsequent stages.

Referenced by Initialize(), WsfTBM_Mover::Initialize2(), ProcessInput(), and Stage().

◆ mIgnitionState

double WsfTBM_Mover::Stage::mIgnitionState[9]

Referenced by WsfTBM_Mover::ComputeTransitionStateVectors(), WsfTBM_Mover::Initialize2(), and Stage().

◆ mIgnitionTime

double WsfTBM_Mover::Stage::mIgnitionTime

The time relative to launch and state when the engine ignites.

Referenced by WsfTBM_Mover::ComputeTransitionStateVectors(), Initialize(), WsfTBM_Mover::Initialize2(), WsfTBM_Mover::ScheduleScriptEvents(), and Stage().

◆ mInitialState

double WsfTBM_Mover::Stage::mInitialState[9]

Referenced by WsfTBM_Mover::ComputeTransitionStateVectors(), and Stage().

◆ mInitialTime

double WsfTBM_Mover::Stage::mInitialTime

The time relative to launch and state when the stage comes into existence (previous stage separates).

Referenced by WsfTBM_Mover::ComputeTransitionStateVectors(), Initialize(), WsfTBM_Mover::Initialize2(), and Stage().

◆ mPayloadMass

double WsfTBM_Mover::Stage::mPayloadMass

Referenced by WsfTBM_Mover::Initialize(), RemainingBurnoutMass(), RemainingInitialMass(), and Stage().

◆ mPreIgnitionCoastTime

double WsfTBM_Mover::Stage::mPreIgnitionCoastTime

Coast time between separation of previous state and ignition of this stage.

Note: A pre-burn coast time for the first stage is not supported.

Referenced by Initialize(), ProcessInput(), and Stage().

◆ mPreSeparationCoastTime

double WsfTBM_Mover::Stage::mPreSeparationCoastTime

Coast time from burnout of this stage to separation.

Note: This is effectively ignored for the last stage.

Referenced by Initialize(), ProcessInput(), and Stage().

◆ mReferenceArea

double WsfTBM_Mover::Stage::mReferenceArea

Reference area.

Referenced by Initialize2(), ProcessInput(), and Stage().

◆ mS_Cd0

double WsfTBM_Mover::Stage::mS_Cd0

The surface area times the drag coefficient (m^2).

Referenced by WsfTBM_Mover::Initialize2(), Initialize2(), and Stage().

◆ mSeparationTime

double WsfTBM_Mover::Stage::mSeparationTime

The time relative to launch when the stage separates from the vehicle.

Referenced by WsfTBM_Mover::ComputeTransitionStateVectors(), Initialize(), WsfTBM_Mover::Initialize2(), WsfTBM_Mover::ScheduleScriptEvents(), and Stage().

◆ mSpecificImpulse

double WsfTBM_Mover::Stage::mSpecificImpulse

The specific impulse (sec).

Referenced by Initialize(), WsfTBM_Mover::Initialize2(), ProcessInput(), and Stage().

◆ mThrust

double WsfTBM_Mover::Stage::mThrust

The thrust (N).

Referenced by Initialize(), WsfTBM_Mover::Initialize2(), ProcessInput(), and Stage().

◆ mThrustDuration

double WsfTBM_Mover::Stage::mThrustDuration

The engine burn time (sec).

Referenced by Initialize(), ProcessInput(), WsfTBM_Mover::ScheduleScriptEvents(), and Stage().

◆ mTotalMass

double WsfTBM_Mover::Stage::mTotalMass

The total mass of the THIS stage (empty mass plus fuel mass).

Note: This does NOT include the mass of the subsequent stages.

Referenced by Initialize(), WsfTBM_Mover::Initialize2(), ProcessInput(), and Stage().

◆ mWdot

double WsfTBM_Mover::Stage::mWdot

The time-rate-of-change of the vehicles weight (NOT MASS) while the engine of this stage is burning.

Referenced by Initialize(), WsfTBM_Mover::Initialize2(), and Stage().

The documentation for this class was generated from the following files:

Public Member Functions

Input values

Derived values

Detailed Description

Constructor & Destructor Documentation

◆ Stage()

Member Function Documentation

◆ Initialize()

◆ Initialize2()

◆ ProcessInput()

◆ RemainingBurnoutMass()

◆ RemainingInitialMass()

Member Data Documentation

◆ mBallisticCoeff

◆ mBurnOutState

◆ mBurnOutTime

◆ mCd0

◆ mEmptyMass

◆ mFuelMass

◆ mFuelMassFraction

◆ mIgnitionState

◆ mIgnitionTime

◆ mInitialState

◆ mInitialTime

◆ mPayloadMass

◆ mPreIgnitionCoastTime

◆ mPreSeparationCoastTime

◆ mReferenceArea

◆ mS_Cd0

◆ mSeparationTime

◆ mSpecificImpulse

◆ mThrust

◆ mThrustDuration

◆ mTotalMass

◆ mWdot