WsfGuidanceComputer::State Class Reference

#include <WsfGuidanceComputer.hpp>

Public Member Functions
	State ()

Public Attributes
double	mSimTime
double	mCurTime
	The simulation time of the start of the current integration interval.
double	mEndTime
	The simulation time of the end of the current integration interval.

The perceived kinematic state of the weapon that the computer is guiding.
UtEntity	mWpnState
double	mFlightPathAngle
	Based on velocity vector, not orientation.
double	mWpnHeading
	Based on velocity vector, not orientation.

The perceived kinematic state of the target to which the computer is guiding.
UtEntity	mTgtState
double	mAimRelLocWCS [3]
double	mAimUnitVecECS [3]
bool	mAimpointIsValid
bool	mAimpointIsTarget

Detailed Description

'State' represents the state of the objects (weapon and target). It is passed to the guidance programs where they are used in evaluation.

Constructor & Destructor Documentation

State()

WsfGuidanceComputer::State::State ( )

inline

References mAimpointIsTarget, mAimpointIsValid, mAimRelLocWCS, mAimUnitVecECS, mCurTime, mEndTime, mFlightPathAngle, mSimTime, mTgtState, mWpnHeading, and mWpnState.

Member Data Documentation

mAimpointIsTarget

bool WsfGuidanceComputer::State::mAimpointIsTarget

Referenced by State().

mAimpointIsValid

bool WsfGuidanceComputer::State::mAimpointIsValid

Referenced by State().

mAimRelLocWCS

double WsfGuidanceComputer::State::mAimRelLocWCS[3]

Referenced by WsfGuidanceProgram::ProNavGuidance(), WsfGuidanceProgram::PursuitGuidance(), and State().

mAimUnitVecECS

double WsfGuidanceComputer::State::mAimUnitVecECS[3]

Referenced by WsfGuidanceProgram::PursuitGuidance(), and State().

mCurTime

double WsfGuidanceComputer::State::mCurTime

The simulation time of the start of the current integration interval.

Referenced by WsfGuidanceProgram::AltitudeGuidance(), WsfGuidanceProgram::AngleOffsetGuidance(), WsfGuidanceProgram::FlightPathAngleGuidance(), and State().

mEndTime

double WsfGuidanceComputer::State::mEndTime

The simulation time of the end of the current integration interval.

Referenced by WsfGuidanceProgram::AngleOffsetGuidance(), WsfGuidanceProgram::FlightPathAngleGuidance(), and State().

mFlightPathAngle

double WsfGuidanceComputer::State::mFlightPathAngle

Based on velocity vector, not orientation.

Referenced by WsfGuidanceProgram::AltitudeGuidance(), WsfGuidanceProgram::FlightPathAngleAchieved(), WsfGuidanceProgram::FlightPathAngleGuidance(), and State().

mSimTime

double WsfGuidanceComputer::State::mSimTime

The current simulation time. This is the final time to which the mover is trying to achieve. It typically moves forward in smaller integration intervals. Note that mCurTime < mEndTime <= mSimTime.

Referenced by State().

mTgtState

UtEntity WsfGuidanceComputer::State::mTgtState

Referenced by WsfGuidanceProgram::AngleOffsetGuidance(), WsfGuidanceProgram::ProNavGuidance(), and State().

mWpnHeading

double WsfGuidanceComputer::State::mWpnHeading

Based on velocity vector, not orientation.

Referenced by WsfGuidanceProgram::AngleOffsetGuidance(), and State().

mWpnState

UtEntity WsfGuidanceComputer::State::mWpnState

Referenced by WsfGuidanceProgram::AngleOffsetGuidance(), WsfGuidanceProgram::FlightPathAngleGuidance(), WsfGuidanceProgram::ProNavGuidance(), and State().

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

• WsfGuidanceComputer.hpp