#include <BrawlerMover.hpp>

Inheritance diagram for BrawlerMover:

Collaboration diagram for BrawlerMover:

Public Types
enum	CommandType { RATES = 1 , HEADING_SPEED_ALTITUDE = 2 , PLANE_GEES_SPEED = 3 , VECTOR_GEES = 4 , ALSO_COMMAND_ALPHA = 9 }

Public Member Functions
	BrawlerMover ()
BrawlerMover &	operator= (const BrawlerMover &)=delete
virtual	~BrawlerMover ()
virtual bool	LoadAeroConfig (const std::string &absolutePathFile)
virtual bool	Initialize (double aCreationTime, UtEntity &aStartingState, BrawlerPlatform *aPlatformPtr)
virtual bool	UpdateState (double toSimTime)
virtual UtEntity	State (double aSimTime)
virtual void	DeleteMover ()=0
virtual void	UpdateFuel (double aTimeStep, double aInitialFlow, double aThrottle, double &aFuelQuantity, double &aVehicleMass)
virtual double	PlatformTime ()
virtual UtVec3d &	Position ()
virtual double	Altitude ()
virtual UtVec3d &	Velocity ()
virtual UtVec3d &	Acceleration ()
virtual UtFortMat3d &	EarthToBodyRotationMatrix ()
virtual UtFortMat3d &	EarthToWindRotationMatrix ()
virtual UtVec3d &	AngularRates ()
virtual double	Alpha ()
virtual double	AlphaCL0 ()
virtual double	AngleOfAttackRate ()
virtual double	AircraftMass ()
virtual double	EmptyMass ()
virtual double	Speed ()
virtual double	TurnRadius ()
virtual double	Mach ()
virtual double	DynamicPressure ()
virtual double	LagFilterFreqPitchRate ()
virtual double	LagFilterFreqRollRate ()
virtual double	RollRateMax ()
virtual double	PitchRatePositiveMax ()
virtual double	RollMax ()
virtual double	ReferenceArea ()
virtual double	Gas ()
virtual double	MaxAllowedThrottle ()
virtual double	CoefficientOfLift (double mach, double alpha)
virtual double	CoefficientOfDrag (double mach, double alpha)
virtual double	Drag2 ()
virtual double	Drag (double alpha, double speed, double altitude)
virtual double	Lift ()
virtual double	Lift (double alpha, double speed, double altitude)
virtual double	LiftFromAlpha (double alpha)
virtual double	AngleOfAttackFromDrag (double drag)
virtual double	AngleOfAttackFromLift (double lift)
virtual double	CalibratedAirSpeed ()
virtual double	SpecificEnergyRate ()
	Returns specific energy rate calculated in aproj3.
virtual double	Thrust (double throttle)
virtual double	Thrust (double throttle, double speed, double altitude)
virtual double	Throttle ()
virtual double	AxialForceX ()
virtual double	InletDrag (double throttle)
virtual UtVec3d	VelocityWindAxes (void)
virtual UtVec3d	GravityWindAxes (void)
virtual UtVec3d	AccelerationWindAxes (void)
void	CommandRates (UtVec3d &aAngularRates, UtVec3d &aLongitudinalAccel)
void	CommandHeadingSpeedAltitude (double aHeading, double aSpeed, double aAltitude, double aMaxGees, double aMaxClimb)
void	CommandPlaneManeuver (const UtVec3d &aPlane, double aGees, double aSpeed, bool aThrottleFlag=false)
void	CommandVector (UtVec3d &aVelocityVector, double aMaxGees, double aSpeed, bool aThrottleFlag=false)
void	CommandLevelTurn (double aHeading, double aMach, double aGees)
void	CommandSlice (double aHeading, double aAltitude, double aRunMach)
void	prlevl (double aGees, double aTurn, double aRoc, double aHeading, double aMach)
void	forcev (double spd, std::string spdmod, double headng, double rclimb)
void	dirct (double spddes, std::string spdmd, double rolds, std::string rolmd, double geedes)
void	SetMaxThrottle (double aThrottle)
void	aproj3 (double timeDelta, UtEntity &proj)
void	allim (double aldes, double alpha, double cosalf, double gx, double acm, double &along, double &thrust)
void	grthr (double aldes, double drag, double cosaoa, double gx, double &grosst, double &epd)
void	laccel (double &along, double almin_use, UtVec3d &atrans, const UtVec3d &v, double spd, const UtFortMat3d &rbe, double acm, double amax, double &atload, double &erate)
void	prjacc (const UtVec3d &xin, const UtVec3d &vin, const UtVec3d &a, double dt, UtVec3d &xout, UtVec3d &vout)
void	spdtoa (double spd0x, double spdtmp, double dspeed, const UtVec3d &vdes, double dt, double gmax, const UtVec3d &vtemp, double &aldes, UtVec3d &atrans)
void	thstoa (double gx, double frclon, const UtVec3d &dir0, const UtVec3d &vtemp, double spdtmp, double dt, double gmax, double &aldes, UtVec3d &atrans)
void	manwnd (const UtVec3d &v, const UtVec3d &a, UtFortMat3d &rw, double &al, double &at)
void	perfrm ()
double	corner (double alt, double vs, double wate)
void	flyac (double toTime)
void	rates (double &xl, double thrst, double &dt, double tend, UtVec3d &wact, double &spddes, UtVec3d &vw, UtVec3d &gw, UtVec3d &aw, const int arotyp, double &aoaact, double &aldact)
void	gwreq (double &dt, double thrst, double tend, UtVec3d &aw, UtVec3d &wnext, double &spddes, double &aoades, bool &gavdfl)
void	flact1 (UtVec3d &wnext, double &d, double delt, double &flow, double spddes, double &faxial, double &wate, double &xl, double &efpd)
void	seteng (double delt, double drg, double spddes, double tsmn)
void	desaxf (double drg, double spddes, double tsmn, double &axfreq, double &accx)
void	flacti (double &faxial, double &xl, double &flow, double &efpd)
void	flyac_short (double dt)
void	flact0 (UtVec3d &vw, UtVec3d &gw, UtVec3d &aw)
void	acarea ()
void	getdt (UtVec3d &aw, UtVec3d &wnow, double ftim, double &dt)
void	ratmx1 (double xl, double acmass, UtVec3d &avw, UtVec3d &agw, double aoaold, double thrst, double &maxp, double &qmxpos, double &qmxneg, double &aoamx)
double	pmax (double wate, double glift)
double	gliftm (double mach, double dypr, double wate)
double	fliftm (double mach, double dypr, double wate)
double	qmax (double u, double wate, double awz, const int idir)
void	aoamx1 (double acmass, double &aoamx)
double	actxdt (double xdota0, double xdotr, double omeg, double dt)
double	gldmx (double wate, const int idir)
double	dsxdot (double xdes, double x, double xdot, double xdotmx, double tau)
double	stept (double ades, double w, double angmax, double &wdes, double tau)
void	qroots (double a, double b, double c, double &x1, double &x2, bool &solutn)
bool	toltst (double xf, double x0, double tol)
void	adjal (double &aly, double &alz, double &al, double greqm, UtVec3d &toup, bool &gavdfl)
void	altlim (UtVec3d &vwr)
void	vmake2 (double a, UtVec3d &vin, UtVec3d &vout)
void	chkrng (double x, double xmin, double xmax, std::string text)
void	ckrngi (const int k, const int kmin, const int kmax, const std::string &text)
void	desang (UtVec3d &vw, UtVec3d &wnow, double &cphi, double &sphi, double &psidot, double &psi)
void	orient (UtFortMat3d &dircos, double &yaw, double &pitch, double &roll)
void	rollim (UtVec3d &gw, double &roldes, double &aly, double &alz, double psi)
void	limchk (double value, double limit, double maxovr, double minund, double timnow, double &toact, double &timovr, double &timund, bool &ld2, bool &over, bool limon)
void	udrbe (UtFortMat3d &rbe, UtVec3d &w, double wsq, double wmag, double chi)
void	udxv (UtVec3d &accbar, UtVec3d &pos, UtVec3d &vel, double delt, UtFortMat3d &rwea)
double	fflo (double thrtlx)
void	getqm (double speed, double &dyp, double &fmach)
void	deseng (double freq, double &fggdes, double &fabdes, double &ddpdes, double &trpdes)
double	throt (double thrst)
void	stenst (double fggdes, double fabdes, double ddpdes, double trpdes, double delt)
void	effth2 (double thrtlx, double &efgrth, double &efpd)
void	effthr (double fggc, double fabc, double trpdc, double ddpdc, double &efgrth, double &efpd)
void	thrst2 (double fgg, double fab, double &tgg, double &tab, double &id)
void	max_asubt (double &g_trans_max, bool &low_spd)
double	drag (double tlift)
double	drag2 (double xaoa)
double	fdrag2 (double xaoa, const int num_acd_m, double acd_mach, double acd)
double	fdrag_inner (double aoa, const int num_acd_m, double acd_mach, double acd)
void	gcdadd (const int num_mach, double machs, double cds, double &cdadd)
double	drgad ()
double	xlift (double alfa)
double	fxlift (double alfa)
double	get_aoa (double drag)
void	srch2 (double *x, const int nx, double xint, int &ilow, double &p)
double	cas (double speed)
void	atmos (double alt, double &t, double &pres, double &dens, double &vs, double &pr, double &dr)
void	thrust (double thrtlx, double &tgg, double &tab, double &id)
void	thrdec (double thrtlx, double &fgg, double &fab, double &trpd)
void	thrst3 (double fgg, double fab, double &tgg, double &tab, double &id, double trpd, bool destrv)
void	fthrst (double fgg, double fab, double &tgg, double &tab, double &id)
void	fntthr (double fgg, double fab, double &tgg, double &tab)
double	susgmx (double wate, double thrtlx)
double	aoamcl (double wate)
double	aoa (double xl, bool postall)
double	faoa (double xl, bool postall)

Public Attributes
UtVec3d	mAngularRates
UtVec3d	mAxialAccel
UtVec3d	mPlane
UtVec3d	mVelocityVector
double	mHeading
double	mAltitude
double	mSpeed
double	mThrottle
double	mMaxGees
double	mMaxClimb
CommandType	mCommandType
bool	mThrottleFlag
UtVec3d	gravec
double	tsv
UtVec3d	pos
UtVec3d	vel
UtVec3d	acc
UtFortMat3d	rbea
UtFortMat3d	rwea
UtVec3d	wnow
double	alfa
double	alfdot
double	amass
double	spd
double	turn
double	wsqr
double	rate
double	fm
double	bvrmch
double	dyp
double	omegp
double	omegq
double	pmx
double	qmxpos
double	rlthrs
double	rolmx
double	rarea
double	gas
double	tset
double	ttset
double	fggsv
double	fabsv
double	trpdsv
double	ddpdsv
double	mxexrl
double	mnonrl
double	tmexrl
double	tmonrl
double	tmacex
bool	ld2
bool	over
double	svtime
double	barems
double	crnrv
double	fmmax
double	casmax
double	trefgg
double	trmla
double	abdt
double	dtggup
double	dtggdn
bool	tdlim
bool	tmlim
bool	tablim
double	trmm
double	trtd
double	alpha0
int	aoa_tab_type
int	nfm1
int	nfm2
int	nfm3
double	fmvec1 [mfm]
double	fmvec2 [mfm]
double	fmvec3 [mfm]
double	clmax [mfm]
int	nalph1
int	nalph2
double	alfv1 [malpha]
double	alfv2 [malpha]
double	clift [mfm *malpha]
double	cdrag [mfm *malpha]
int	nmach1
int	nhts
double	mchval [mmach1]
double	htvec [mhts]
double	tidle [mmach1 *mhts]
double	tmil [mmach1 *mhts]
double	thrmx [mmach1 *mhts]
double	abcorl
double	gcap [2][mmach1]
double	gcap2 [2][mmach1]
double	rfarea [msweep]
double	floidl [mmach1 *mhts]
double	flomil [mmach1 *mhts]
double	flomax [mmach1 *mhts]
double	ff_adj
double	dragvl [ndatbl]
double	aoavl [ndatbl]
double	drgaoa [ndtbl2]
UtVec3d	aw
UtVec3d	gwind
double	almax
double	almin
double	gmxin
double	thrmin
double	thrnow
double	thrmax
double	drgnow
double	gmxsu
double	almaxg
double	alming
double	amxin
double	drgsu
double	wmax
double	wate
double	gmnin
double	gmxsut
double	psubs
double	cornrv
double	tempme
double	presme
double	densme
double	vsme
double	prme
double	drme
double	radmnp
double	aoamx
double	aoamn
double	epdmin
double	epdnow
double	epdmax
double	thrstl [5]
double	throtm
double	altmin
double	altmax
double	casmin
double	miss_mass
double	parea [3]
double	deswt
double	ac_fuel_cap
int	arotyp
double	thrst_adj
int	num_ac_acd_m
double	ac_acd_mach [2 *max_acd_mach]
double	ac_acd [2 *max_acd_mach]
double	throtl
bool	aeroLoaded
BrawlerPlatform *	mBrawlerPlatformPtr

Protected Member Functions
	BrawlerMover (const BrawlerMover &aSrc)

Member Enumeration Documentation

◆ CommandType

enum BrawlerMover::CommandType

Enumerator
RATES
HEADING_SPEED_ALTITUDE
PLANE_GEES_SPEED
VECTOR_GEES
ALSO_COMMAND_ALPHA

Constructor & Destructor Documentation

◆ BrawlerMover() [1/2]

BrawlerMover::BrawlerMover ( const BrawlerMover & aSrc )

protected

References abcorl, abdt, ac_acd, ac_acd_mach, ac_fuel_cap, acc, aeroLoaded, alfa, alfdot, alfv1, alfv2, almax, almaxg, almin, alming, alpha0, altmax, altmin, amass, amxin, aoa_tab_type, aoamn, aoamx, aoavl, arotyp, aw, barems, BrawlerMover(), bvrmch, casmax, casmin, cdrag, clift, clmax, cornrv, crnrv, ddpdsv, densme, deswt, dragvl, drgaoa, drgnow, drgsu, drme, dtggdn, dtggup, dyp, epdmax, epdmin, epdnow, fabsv, ff_adj, fggsv, floidl, flomax, flomil, fm, fmmax, fmvec1, fmvec2, fmvec3, gas, gcap, gcap2, gmnin, gmxin, gmxsu, gmxsut, gravec, gwind, htvec, ld2, mAltitude, mAngularRates, mAxialAccel, mBrawlerPlatformPtr, mchval, mCommandType, mHeading, miss_mass, mMaxClimb, mMaxGees, mnonrl, mPlane, mSpeed, msweep, mThrottle, mThrottleFlag, mVelocityVector, mxexrl, nalph1, nalph2, ndatbl, ndtbl2, nfm1, nfm2, nfm3, nhts, nmach1, num_ac_acd_m, omegp, omegq, over, parea, pmx, pos, presme, prme, psubs, qmxpos, radmnp, rarea, rate, rbea, rfarea, rlthrs, rolmx, rwea, spd, svtime, tablim, tdlim, tempme, thrmax, thrmin, thrmx, thrnow, throtl, throtm, thrst_adj, thrstl, tidle, tmacex, tmexrl, tmil, tmlim, tmonrl, trefgg, trmla, trmm, trpdsv, trtd, tset, tsv, ttset, turn, vel, vsme, wate, wmax, wnow, and wsqr.

Referenced by BrawlerMover(), operator=(), WsfBrawlerMover::WsfBrawlerMover(), and WsfBrawlerMover::WsfBrawlerMover().

◆ BrawlerMover() [2/2]

BrawlerMover::BrawlerMover ( )

References abcorl, abdt, ac_acd, ac_acd_mach, ac_fuel_cap, acc, aero1, aeroLoaded, alfa, alfdot, alfv1, alfv2, almax, almaxg, almin, alming, alpha0, altmax, altmin, amass, amxin, aoa_tab_type, aoamn, aoamx, aoavl, arotyp, aw, barems, bvrmch, casmax, casmin, cdrag, clift, clmax, cornrv, crnrv, ddpdsv, densme, deswt, dragvl, drgaoa, drgnow, drgsu, drme, dtggdn, dtggup, dyp, epdmax, epdmin, epdnow, fabsv, ff_adj, fggsv, floidl, flomax, flomil, fm, fmmax, fmvec1, fmvec2, fmvec3, gas, gcap, gcap2, gmnin, gmxin, gmxsu, gmxsut, BRAWLER::grav, gravec, gwind, htvec, ld2, mAltitude, mAngularRates, mAxialAccel, mBrawlerPlatformPtr, mchval, mCommandType, mHeading, miss_mass, mMaxClimb, mMaxGees, mnonrl, mPlane, mSpeed, mThrottle, mThrottleFlag, mVelocityVector, mxexrl, nalph1, nalph2, ndatbl, ndtbl2, nfm1, nfm2, nfm3, nhts, nmach1, num_ac_acd_m, omegp, omegq, over, parea, pmx, pos, presme, prme, psubs, qmxpos, BRAWLER::rad, radmnp, rarea, rate, RATES, rbea, reflective, rfarea, rlthrs, rolmx, rwea, spd, svtime, tablim, tdlim, tempme, thrmax, thrmin, thrmx, thrnow, throtl, throtm, thrst_adj, thrstl, tidle, tmacex, tmexrl, tmil, tmlim, tmonrl, trefgg, trmla, trmm, trpdsv, trtd, tset, tsv, ttset, turn, vel, vsme, wate, wmax, wnow, wsqr, and BRAWLER::xlarge.

◆ ~BrawlerMover()

BrawlerMover::~BrawlerMover ( )

virtual

Member Function Documentation

◆ acarea()

void BrawlerMover::acarea ( )

References rarea, and rfarea.

Referenced by flyac().

◆ Acceleration()

virtual UtVec3d & BrawlerMover::Acceleration ( )

inlinevirtual

References acc.

Referenced by aproj3(), dirct(), flact0(), and perfrm().

◆ AccelerationWindAxes()

UtVec3d BrawlerMover::AccelerationWindAxes ( void )

virtual

References acc, and rwea.

Referenced by aproj3().

◆ actxdt()

double BrawlerMover::actxdt	(	double	xdota0,
		double	xdotr,
		double	omeg,
		double	dt )

References actxdt().

Referenced by actxdt(), and rates().

◆ adjal()

void BrawlerMover::adjal	(	double &	aly,
		double &	alz,
		double &	al,
		double	greqm,
		UtVec3d &	toup,
		bool &	gavdfl )

References Altitude(), BRAWLER::grav, BRAWLER::makecs(), rwea, and vel.

Referenced by gwreq().

◆ AircraftMass()

virtual double BrawlerMover::AircraftMass ( )

inlinevirtual

References amass.

Referenced by WsfBrawlerMover::ReasonableClimbRate().

◆ allim()

void BrawlerMover::allim	(	double	aldes,
		double	alpha,
		double	cosalf,
		double	gx,
		double	acm,
		double &	along,
		double &	thrust )

References aoamx, drgaoa, grthr(), ndtbl2, BRAWLER::tbl1b(), and thrust().

Referenced by aproj3(), and laccel().

◆ Alpha()

virtual double BrawlerMover::Alpha ( )

inlinevirtual

References alfa.

Referenced by Lift(), perfrm(), and WsfBrawlerMover::ReasonableClimbRate().

◆ AlphaCL0()

virtual double BrawlerMover::AlphaCL0 ( )

inlinevirtual

References alpha0.

◆ Altitude()

virtual double BrawlerMover::Altitude ( )

inlinevirtual

References Position().

Referenced by adjal(), altlim(), cas(), CommandSlice(), fflo(), fntthr(), getqm(), gwreq(), WsfBrawlerMover::ReasonableClimbRate(), and WsfBrawlerMover::UpdateRoute().

◆ altlim()

void BrawlerMover::altlim ( UtVec3d & vwr )

References Altitude(), altmax, altmin, BRAWLER::amax1(), BRAWLER::amin1(), mVelocityVector, rwea, Speed(), vel, and vmake2().

Referenced by gwreq().

◆ AngleOfAttackFromDrag()

virtual double BrawlerMover::AngleOfAttackFromDrag ( double drag )

inlinevirtual

References drag(), and get_aoa().

Referenced by max_asubt().

◆ AngleOfAttackFromLift()

virtual double BrawlerMover::AngleOfAttackFromLift ( double lift )

inlinevirtual

References aoa().

◆ AngleOfAttackRate()

virtual double BrawlerMover::AngleOfAttackRate ( )

inlinevirtual

References alfdot.

◆ AngularRates()

virtual UtVec3d & BrawlerMover::AngularRates ( )

inlinevirtual

References wnow.

Referenced by aproj3(), flact1(), flyac(), flyac_short(), gwreq(), rates(), and State().

◆ aoa()

double BrawlerMover::aoa	(	double	xl,
		bool	postall )

References aoa(), faoa(), BRAWLER::nabort(), and undnum.

Referenced by AngleOfAttackFromLift(), aoa(), aoamcl(), dirct(), Drag(), fdrag2(), fdrag_inner(), gwreq(), laccel(), perfrm(), and rates().

◆ aoamcl()

double BrawlerMover::aoamcl ( double wate )

References alfv1, aoa(), clift, fm, fmvec2, fxlift(), gldmx(), nalph1, nfm2, BRAWLER::srch(), and wate.

Referenced by susgmx().

◆ aoamx1()

void BrawlerMover::aoamx1	(	double	acmass,
		double &	aoamx )

References alfv1, BRAWLER::amin1(), aoa_tab_type, aoamx, clift, clmax, DynamicPressure(), fmvec1, fmvec2, gcap, gcap2, BRAWLER::grav, BRAWLER::invtb2(), Mach(), mchval, miss_mass, BRAWLER::nabort(), nalph1, nfm1, nfm2, nmach1, BRAWLER::param1(), ReferenceArea(), reflective, BRAWLER::srch(), BRAWLER::tbl1(), and wate.

Referenced by ratmx1().

◆ aproj3()

void BrawlerMover::aproj3	(	double	timeDelta,
		UtEntity &	proj )

References BrawlerPlatform::a_lim(), Acceleration(), AccelerationWindAxes(), allim(), almaxg, amass, BRAWLER::amax1(), BRAWLER::amin1(), amxin, AngularRates(), aoavl, aw, BRAWLER::bodyax(), casmin, BrawlerCoordinateConversion::ConvertNEDtoLLA(), dragvl, drme, EarthToBodyRotationMatrix(), EarthToWindRotationMatrix(), BRAWLER::grav, gravec, grthr(), gwind, HEADING_SPEED_ALTITUDE, laccel(), BRAWLER::makecs(), BRAWLER::makeh(), mAltitude, mAngularRates, manwnd(), mAxialAccel, mCommandType, mMaxClimb, mMaxGees, mSpeed, mThrottle, mThrottleFlag, mVelocityVector, BRAWLER::nabort(), ndatbl, orient(), BRAWLER::param1(), PLANE_GEES_SPEED, Position(), prjacc(), BrawlerPlatform::projw(), BRAWLER::ramp(), RATES, BRAWLER::sign(), spdtoa(), BRAWLER::tbl1b(), throtm, thrstl, thrust(), thstoa(), udrbe(), VECTOR_GEES, Velocity(), BRAWLER::vorth(), and BRAWLER::xlimit().

Referenced by WsfBrawlerMover::ProjectForward().

◆ atmos()

void BrawlerMover::atmos	(	double	alt,
		double &	t,
		double &	pres,
		double &	dens,
		double &	vs,
		double &	pr,
		double &	dr )

References c1, c6, DeleteMover(), dsl, psl, trkr_neg_alt, and tsl.

Referenced by cas(), Drag(), getqm(), Lift(), perfrm(), and Thrust().

◆ AxialForceX()

virtual double BrawlerMover::AxialForceX ( )

inlinevirtual

References flacti().

◆ CalibratedAirSpeed()

virtual double BrawlerMover::CalibratedAirSpeed ( )

inlinevirtual

References cas(), and Speed().

◆ cas()

double BrawlerMover::cas ( double speed )

References Altitude(), atmos(), DeleteMover(), BRAWLER::nabort(), BRAWLER::tbl2e(), and trkr_neg_alt.

Referenced by CalibratedAirSpeed(), corner(), desaxf(), forcev(), and max_asubt().

◆ chkrng()

void BrawlerMover::chkrng	(	double	x,
		double	xmin,
		double	xmax,
		std::string	text )

References BRAWLER::nabort().

Referenced by fflo(), fntthr(), fthrst(), thrdec(), thrst3(), and toltst().

◆ ckrngi()

void BrawlerMover::ckrngi	(	const int	k,
		const int	kmin,
		const int	kmax,
		const std::string &	text )

References BRAWLER::nabort().

Referenced by gwreq().

◆ CoefficientOfDrag()

double BrawlerMover::CoefficientOfDrag	(	double	mach,
		double	alpha )

virtual

References alfv2, cdrag, fmvec3, nalph2, nfm3, and BRAWLER::tbl2e().

Referenced by Drag(), and fdrag_inner().

◆ CoefficientOfLift()

double BrawlerMover::CoefficientOfLift	(	double	mach,
		double	alpha )

virtual

◆ CommandHeadingSpeedAltitude()

void BrawlerMover::CommandHeadingSpeedAltitude	(	double	aHeading,
		double	aSpeed,
		double	aAltitude,
		double	aMaxGees,
		double	aMaxClimb )

References HEADING_SPEED_ALTITUDE, mAltitude, mCommandType, mHeading, mMaxClimb, mMaxGees, mSpeed, and mThrottleFlag.

Referenced by WsfBrawlerMover::FlyHeadingSpeedAltitude(), WsfBrawlerMover::GoToAltitude(), WsfBrawlerMover::GoToLocation(), WsfBrawlerMover::GoToSpeed(), WsfBrawlerMover::TurnToHeading(), and WsfBrawlerMover::Update().

◆ CommandLevelTurn()

void BrawlerMover::CommandLevelTurn	(	double	aHeading,
		double	aMach,
		double	aGees )

References gmxsut, and prlevl().

Referenced by WsfBrawlerMover::Prlvl(), and WsfBrawlerMover::Prlvlg().

◆ CommandPlaneManeuver()

void BrawlerMover::CommandPlaneManeuver	(	const UtVec3d &	aPlane,
		double	aGees,
		double	aSpeed,
		bool	aThrottleFlag = false )

References mCommandType, mMaxGees, mPlane, mSpeed, mThrottle, mThrottleFlag, and PLANE_GEES_SPEED.

Referenced by dirct(), WsfBrawlerMover::TurnInPlaneWithSpeed(), and WsfBrawlerMover::TurnInPlaneWithThrottle().

◆ CommandRates()

void BrawlerMover::CommandRates	(	UtVec3d &	aAngularRates,
		UtVec3d &	aLongitudinalAccel )

References mAngularRates, mAxialAccel, mCommandType, and RATES.

Referenced by WsfBrawlerMover::FlyRates().

◆ CommandSlice()

void BrawlerMover::CommandSlice	(	double	aHeading,
		double	aAltitude,
		double	aRunMach )

References Altitude(), BRAWLER::amin1(), aw, bvrmch, dirct(), EarthToBodyRotationMatrix(), fm, forcev(), gmxsut, BRAWLER::grav, gravec, BRAWLER::headeg(), orient(), BRAWLER::rad, BRAWLER::ramp(), BRAWLER::sign(), Velocity(), and BRAWLER::xlimit().

Referenced by WsfBrawlerMover::Slice().

◆ CommandVector()

void BrawlerMover::CommandVector	(	UtVec3d &	aVelocityVector,
		double	aMaxGees,
		double	aSpeed,
		bool	aThrottleFlag = false )

References mCommandType, mMaxGees, mSpeed, mThrottle, mThrottleFlag, mVelocityVector, and VECTOR_GEES.

Referenced by WsfBrawlerMover::FlyVectorWithSpeed(), WsfBrawlerMover::FlyVectorWithThrottle(), and forcev().

◆ corner()

double BrawlerMover::corner	(	double	alt,
		double	vs,
		double	wate )

References BRAWLER::amin1(), cas(), casmax, clmax, crnrv, fmvec1, gcap, gcap2, getqm(), gliftm(), BRAWLER::grav, mchval, miss_mass, nfm1, nmach1, spd, BRAWLER::tbl1(), wate, and BRAWLER::xlarge.

Referenced by perfrm().

◆ DeleteMover()

virtual void BrawlerMover::DeleteMover ( )

pure virtual

Implemented in WsfBrawlerMover.

References UpdateFuel().

Referenced by atmos(), cas(), and UpdateFuel().

◆ desang()

void BrawlerMover::desang	(	UtVec3d &	vw,
		UtVec3d &	wnow,
		double &	cphi,
		double &	sphi,
		double &	psidot,
		double &	psi )

References wnow.

Referenced by gwreq().

◆ desaxf()

void BrawlerMover::desaxf	(	double	drg,
		double	spddes,
		double	tsmn,
		double &	axfreq,
		double &	accx )

References alfa, ALSO_COMMAND_ALPHA, amass, cas(), casmax, effth2(), fmmax, gravec, HEADING_SPEED_ALTITUDE, Mach(), mAxialAccel, mCommandType, mThrottleFlag, BRAWLER::nabort(), PLANE_GEES_SPEED, RATES, rwea, Speed(), tdlim, trefgg, trmla, and VECTOR_GEES.

Referenced by seteng().

◆ deseng()

void BrawlerMover::deseng	(	double	freq,
		double &	fggdes,
		double &	fabdes,
		double &	ddpdes,
		double &	trpdes )

References alfa, amass, effth2(), BRAWLER::grav, grthr(), Mach(), BRAWLER::nabort(), thrdec(), throt(), thrst2(), tmlim, trefgg, trmm, and BRAWLER::xlimit().

Referenced by seteng().

◆ dirct()

void BrawlerMover::dirct	(	double	spddes,
		std::string	spdmd,
		double	rolds,
		std::string	rolmd,
		double	geedes )

References Acceleration(), amass, aoa(), CommandPlaneManeuver(), drag(), dyp, effth2(), fm, getqm(), BRAWLER::grav, gravec, grthr(), BRAWLER::makcsi(), BRAWLER::makex(), BRAWLER::mrotx(), orient(), BRAWLER::rad, BRAWLER::sign(), Speed(), throt(), Velocity(), and BRAWLER::xlimit().

Referenced by CommandSlice(), and prlevl().

◆ Drag()

double BrawlerMover::Drag	(	double	alpha,
		double	speed,
		double	altitude )

virtual

References ac_acd, ac_acd_mach, aoa(), atmos(), CoefficientOfDrag(), drag(), gcdadd(), num_ac_acd_m, and ReferenceArea().

Referenced by WsfBrawlerMover::ReasonableClimbRate().

◆ drag()

double BrawlerMover::drag ( double tlift )

Referenced by AngleOfAttackFromDrag(), dirct(), Drag(), fdrag_inner(), get_aoa(), grthr(), perfrm(), and WsfBrawlerMover::ReasonableClimbRate().

◆ Drag2()

virtual double BrawlerMover::Drag2 ( )

inlinevirtual

References alpha0, and drag2().

◆ drag2()

double BrawlerMover::drag2 ( double xaoa )

References ac_acd, ac_acd_mach, drag2(), fdrag2(), BRAWLER::nabort(), num_ac_acd_m, and undnum.

Referenced by Drag2(), drag2(), flact1(), max_asubt(), perfrm(), and susgmx().

◆ drgad()

double BrawlerMover::drgad ( )

References BRAWLER::nabort().

◆ dsxdot()

double BrawlerMover::dsxdot	(	double	xdes,
		double	x,
		double	xdot,
		double	xdotmx,
		double	tau )

References dsxdot(), and BRAWLER::sign().

Referenced by dsxdot(), and gwreq().

◆ DynamicPressure()

virtual double BrawlerMover::DynamicPressure ( )

inlinevirtual

References dyp.

Referenced by aoamx1(), faoa(), fdrag2(), fdrag_inner(), fxlift(), get_aoa(), gldmx(), WsfBrawlerProcessor::MaxInstantaneousGLoad_g(), pmax(), qmax(), and rates().

◆ EarthToBodyRotationMatrix()

virtual UtFortMat3d & BrawlerMover::EarthToBodyRotationMatrix ( )

inlinevirtual

References rbea.

Referenced by aproj3(), and CommandSlice().

◆ EarthToWindRotationMatrix()

virtual UtFortMat3d & BrawlerMover::EarthToWindRotationMatrix ( )

inlinevirtual

References rwea.

Referenced by aproj3(), flact0(), and perfrm().

◆ effth2()

void BrawlerMover::effth2	(	double	thrtlx,
		double &	efgrth,
		double &	efpd )

References effthr(), and thrdec().

Referenced by desaxf(), deseng(), and dirct().

◆ effthr()

void BrawlerMover::effthr	(	double	fggc,
		double	fabc,
		double	trpdc,
		double	ddpdc,
		double &	efgrth,
		double &	efpd )

References BRAWLER::amax1(), BRAWLER::amin1(), throtm, thrst2(), trefgg, and BRAWLER::xlimit().

Referenced by effth2(), flact1(), flacti(), and perfrm().

◆ EmptyMass()

virtual double BrawlerMover::EmptyMass ( )

inlinevirtual

References barems.

◆ faoa()

double BrawlerMover::faoa	(	double	xl,
		bool	postall )

References alfv1, alpha0, aoa_tab_type, clift, DynamicPressure(), faoa(), fmvec2, BRAWLER::invtb2(), Mach(), BRAWLER::nabort(), nalph1, nfm2, BRAWLER::param1(), ReferenceArea(), reflective, BRAWLER::srch(), and undnum.

Referenced by aoa(), and faoa().

◆ fdrag2()

double BrawlerMover::fdrag2	(	double	xaoa,
		const int	num_acd_m,
		double *	acd_mach,
		double *	acd )

References aoa(), DynamicPressure(), and fdrag_inner().

Referenced by drag2().

◆ fdrag_inner()

double BrawlerMover::fdrag_inner	(	double	aoa,
		const int	num_acd_m,
		double *	acd_mach,
		double *	acd )

References aoa(), CoefficientOfDrag(), drag(), DynamicPressure(), fdrag_inner(), gcdadd(), Mach(), ReferenceArea(), and undnum.

Referenced by fdrag2(), and fdrag_inner().

◆ fflo()

double BrawlerMover::fflo ( double thrtlx )

References Altitude(), chkrng(), ff_adj, fflo(), floidl, flomax, flomil, htvec, Mach(), mchval, nhts, nmach1, BRAWLER::tbl2(), throtm, and undnum.

Referenced by fflo(), flacti(), and UpdateFuel().

◆ flact0()

void BrawlerMover::flact0	(	UtVec3d &	vw,
		UtVec3d &	gw,
		UtVec3d &	aw )

References Acceleration(), aw, EarthToWindRotationMatrix(), gravec, BRAWLER::makecs(), mAxialAccel, mCommandType, mMaxGees, mPlane, PLANE_GEES_SPEED, and Velocity().

Referenced by flyac().

◆ flact1()

void BrawlerMover::flact1	(	UtVec3d &	wnext,
		double &	d,
		double	delt,
		double &	flow,
		double	spddes,
		double &	faxial,
		double &	wate,
		double &	xl,
		double &	efpd )

References acc, alfa, amass, AngularRates(), BRAWLER::bodyax(), ddpdsv, drag2(), dyp, effthr(), fabsv, fggsv, fm, gas, getqm(), BRAWLER::grav, Lift(), mThrottle, pos, rate, rbea, rwea, seteng(), spd, Speed(), trpdsv, tset, udrbe(), udxv(), UpdateFuel(), vel, wate, wnow, and wsqr.

Referenced by flyac().

◆ flacti()

void BrawlerMover::flacti	(	double &	faxial,
		double &	xl,
		double &	flow,
		double &	efpd )

References ddpdsv, effthr(), fabsv, fflo(), fggsv, gas, Lift(), BRAWLER::nabort(), trpdsv, tset, and undnum.

Referenced by AxialForceX(), and flyac().

◆ fliftm()

double BrawlerMover::fliftm	(	double	mach,
		double	dypr,
		double	wate )

References clmax, fmvec1, nfm1, ReferenceArea(), BRAWLER::tbl1(), undnum, and wate.

Referenced by gliftm().

◆ flyac()

void BrawlerMover::flyac ( double toTime )

References acarea(), alfa, alfdot, amass, AngularRates(), arotyp, aw, barems, flact0(), flact1(), flacti(), gas, getdt(), gldmx(), gmxin, BRAWLER::grav, rates(), Speed(), susgmx(), tsv, turn, and wate.

Referenced by UpdateState().

◆ flyac_short()

void BrawlerMover::flyac_short ( double dt )

References acc, alfa, AngularRates(), BRAWLER::bodyax(), pos, rate, rbea, rwea, spd, Speed(), udrbe(), vel, and wsqr.

◆ fntthr()

void BrawlerMover::fntthr	(	double	fgg,
		double	fab,
		double &	tgg,
		double &	tab )

References abcorl, Altitude(), chkrng(), htvec, Mach(), mchval, nhts, nmach1, BRAWLER::tbl2(), thrmx, thrst_adj, tidle, tmil, and undnum.

Referenced by fthrst().

◆ forcev()

void BrawlerMover::forcev	(	double	spd,
		std::string	spdmod,
		double	headng,
		double	rclimb )

References cas(), CommandVector(), fm, gmxsut, BRAWLER::hafpi, BRAWLER::rad, spd, and Speed().

Referenced by CommandSlice(), and prlevl().

◆ fthrst()

void BrawlerMover::fthrst	(	double	fgg,
		double	fab,
		double &	tgg,
		double &	tab,
		double &	id )

References chkrng(), and fntthr().

Referenced by thrst3().

◆ fxlift()

double BrawlerMover::fxlift ( double alfa )

References alfa, alfv1, alpha0, aoa_tab_type, clift, clmax, DynamicPressure(), fmvec1, fmvec2, Mach(), BRAWLER::nabort(), nalph1, nfm1, nfm2, ReferenceArea(), reflective, BRAWLER::sign(), BRAWLER::tbl1(), BRAWLER::tbl2(), undnum, and BRAWLER::xlimit().

Referenced by aoamcl(), and xlift().

◆ Gas()

virtual double BrawlerMover::Gas ( )

inlinevirtual

References gas.

◆ gcdadd()

void BrawlerMover::gcdadd	(	const int	num_mach,
		double *	machs,
		double *	cds,
		double &	cdadd )

References Mach(), and BRAWLER::tbl1().

Referenced by Drag(), and fdrag_inner().

◆ get_aoa()

double BrawlerMover::get_aoa ( double drag )

References alfv2, cdrag, drag(), DynamicPressure(), fmvec3, BRAWLER::invtb2(), Mach(), nalph2, nfm3, BRAWLER::param1(), ReferenceArea(), and srch2().

Referenced by AngleOfAttackFromDrag().

◆ getdt()

void BrawlerMover::getdt	(	UtVec3d &	aw,
		UtVec3d &	wnow,
		double	ftim,
		double &	dt )

References aw, BRAWLER::eps, BRAWLER::rad, and wnow.

Referenced by flyac().

◆ getqm()

void BrawlerMover::getqm	(	double	speed,
		double &	dyp,
		double &	fmach )

References Altitude(), atmos(), drme, and vsme.

Referenced by corner(), dirct(), flact1(), and Initialize().

◆ gldmx()

double BrawlerMover::gldmx	(	double	wate,
		const int	idir )

References BRAWLER::amax1(), BRAWLER::amin1(), DynamicPressure(), fm, gcap, gcap2, gldmx(), gliftm(), BRAWLER::grav, Mach(), mchval, miss_mass, BRAWLER::nabort(), nmach1, BRAWLER::tbl1(), and wate.

Referenced by aoamcl(), flyac(), gldmx(), perfrm(), and rates().

◆ gliftm()

double BrawlerMover::gliftm	(	double	mach,
		double	dypr,
		double	wate )

References fliftm(), BRAWLER::nabort(), undnum, and wate.

Referenced by corner(), gldmx(), WsfBrawlerProcessor::MaxInstantaneousGLoad_g(), pmax(), and qmax().

◆ GravityWindAxes()

UtVec3d BrawlerMover::GravityWindAxes ( void )

virtual

References gravec, and rwea.

◆ grthr()

void BrawlerMover::grthr	(	double	aldes,
		double	drag,
		double	cosaoa,
		double	gx,
		double &	grosst,
		double &	epd )

References amass, drag(), epdmax, epdmin, epdnow, BRAWLER::eps, thrmax, thrmin, thrnow, and BRAWLER::xlimit().

Referenced by allim(), aproj3(), deseng(), dirct(), and laccel().

◆ gwreq()

void BrawlerMover::gwreq	(	double &	dt,
		double	thrst,
		double	tend,
		UtVec3d &	aw,
		UtVec3d &	wnext,
		double &	spddes,
		double &	aoades,
		bool &	gavdfl )

References adjal(), alfa, ALSO_COMMAND_ALPHA, Altitude(), altlim(), amass, BRAWLER::amax1(), BRAWLER::amin1(), AngularRates(), aoa(), aw, BRAWLER::border(), ckrngi(), desang(), dsxdot(), BRAWLER::grav, HEADING_SPEED_ALTITUDE, BRAWLER::makeh(), mAltitude, mAngularRates, max_asubt(), mAxialAccel, mCommandType, mHeading, mMaxClimb, mMaxGees, mSpeed, mThrottleFlag, mVelocityVector, BRAWLER::nabort(), omegp, omegq, pi, PLANE_GEES_SPEED, pmx, qmxpos, BRAWLER::rad, RATES, rollim(), BRAWLER::root2, rwea, BRAWLER::sign(), Speed(), stept(), throtm, toltst(), VECTOR_GEES, and vel.

Referenced by rates().

◆ Initialize()

bool BrawlerMover::Initialize	(	double	aCreationTime,
		UtEntity &	aStartingState,
		BrawlerPlatform *	aPlatformPtr )

virtual

◆ InletDrag()

virtual double BrawlerMover::InletDrag ( double throttle )

inlinevirtual

References InletDrag(), and thrust().

Referenced by InletDrag(), and Thrust().

◆ laccel()

void BrawlerMover::laccel	(	double &	along,
		double	almin_use,
		UtVec3d &	atrans,
		const UtVec3d &	v,
		double	spd,
		const UtFortMat3d &	rbe,
		double	acm,
		double	amax,
		double &	atload,
		double &	erate )

References allim(), amass, BRAWLER::amax1(), BRAWLER::amin1(), amxin, aoa(), aoamx, aoavl, dragvl, BRAWLER::grav, gravec, grthr(), BRAWLER::makecs(), BRAWLER::makeh(), ndatbl, BRAWLER::param1(), BRAWLER::sign(), spd, BRAWLER::srch(), BRAWLER::tbl1b(), thrmax, and BRAWLER::vorth().

Referenced by aproj3().

◆ LagFilterFreqPitchRate()

virtual double BrawlerMover::LagFilterFreqPitchRate ( )

inlinevirtual

References omegp.

◆ LagFilterFreqRollRate()

virtual double BrawlerMover::LagFilterFreqRollRate ( )

inlinevirtual

References omegq.

◆ Lift() [1/2]

virtual double BrawlerMover::Lift ( )

inlinevirtual

References Alpha(), and xlift().

Referenced by flact1(), and flacti().

◆ Lift() [2/2]

double BrawlerMover::Lift	(	double	alpha,
		double	speed,
		double	altitude )

virtual

References alfv1, alpha0, aoa_tab_type, atmos(), clift, clmax, fmvec1, fmvec2, nalph1, nfm1, nfm2, ReferenceArea(), reflective, BRAWLER::sign(), BRAWLER::tbl1(), BRAWLER::tbl2(), and BRAWLER::xlimit().

◆ LiftFromAlpha()

virtual double BrawlerMover::LiftFromAlpha ( double alpha )

inlinevirtual

References xlift().

Referenced by max_asubt(), and susgmx().

◆ limchk()

void BrawlerMover::limchk	(	double	value,
		double	limit,
		double	maxovr,
		double	minund,
		double	timnow,
		double &	toact,
		double &	timovr,
		double &	timund,
		bool &	ld2,
		bool &	over,
		bool	limon )

References ld2, and over.

Referenced by rollim().

◆ LoadAeroConfig()

bool BrawlerMover::LoadAeroConfig ( const std::string & absolutePathFile )

virtual

References abcorl, abdt, ac_fuel_cap, aeroLoaded, alfv1, alfv2, alpha0, aoa_tab_type, barems, casmax, cdrag, clift, clmax, deswt, dtggdn, dtggup, floidl, flomax, flomil, fmmax, fmvec1, fmvec2, fmvec3, gas, gcap, gcap2, BRAWLER::grav, htvec, mchval, miss_mass, msweep, nalph1, nalph2, nfm1, nfm2, nfm3, nhts, nmach1, parea, rarea, BRAWLER::ReadValue(), reflective, rfarea, tablim, tdlim, thrmx, tidle, tmil, tmlim, trefgg, trmla, trmm, trtd, and BRAWLER::TryReadCommand().

Referenced by operator=(), and WsfBrawlerMover::ProcessInput().

◆ Mach()

virtual double BrawlerMover::Mach ( )

inlinevirtual

◆ manwnd()

void BrawlerMover::manwnd	(	const UtVec3d &	v,
		const UtVec3d &	a,
		UtFortMat3d &	rw,
		double &	al,
		double &	at )

References aw, BRAWLER::grav, and BRAWLER::makcsi().

Referenced by aproj3().

◆ max_asubt()

void BrawlerMover::max_asubt	(	double &	g_trans_max,
		bool &	low_spd )

References almin, alpha0, amass, BRAWLER::amin1(), AngleOfAttackFromDrag(), cas(), casmin, drag2(), BRAWLER::grav, gravec, gwind, LiftFromAlpha(), rwea, Speed(), throtm, and thrust().

Referenced by gwreq().

◆ MaxAllowedThrottle()

virtual double BrawlerMover::MaxAllowedThrottle ( )

inlinevirtual

References throtm.

◆ operator=()

BrawlerMover & BrawlerMover::operator= ( const BrawlerMover & )

delete

References BrawlerMover(), Initialize(), LoadAeroConfig(), State(), and UpdateState().

◆ orient()

void BrawlerMover::orient	(	UtFortMat3d &	dircos,
		double &	yaw,
		double &	pitch,
		double &	roll )

References BRAWLER::sign().

Referenced by aproj3(), CommandSlice(), dirct(), and State().

◆ perfrm()

void BrawlerMover::perfrm ( )

References Acceleration(), aero1, BRAWLER::AIMFIRE, almax, almaxg, almin, alming, Alpha(), amass, BRAWLER::amin1(), amxin, aoa(), aoamn, aoamx, aoavl, arotyp, atmos(), aw, corner(), cornrv, ddpdsv, densme, drag(), drag2(), dragvl, drgaoa, drgnow, drgsu, drme, EarthToWindRotationMatrix(), effthr(), epdmax, epdmin, epdnow, fabsv, fggsv, BRAWLER::ftnmi, gldmx(), gmnin, gmxin, gmxsu, gmxsut, BRAWLER::grav, gravec, gwind, BRAWLER::INTERCEPT, Mach(), mBrawlerPlatformPtr, BRAWLER::nabort(), ndatbl, ndtbl2, Position(), presme, prme, psubs, radmnp, susgmx(), tempme, thrmax, thrmin, thrnow, throtm, thrstl, thrust(), trpdsv, Velocity(), vsme, wate, and wmax.

Referenced by UpdateState().

◆ PitchRatePositiveMax()

virtual double BrawlerMover::PitchRatePositiveMax ( )

inlinevirtual

References qmxpos.

◆ PlatformTime()

virtual double BrawlerMover::PlatformTime ( )

inlinevirtual

References tsv.

◆ pmax()

double BrawlerMover::pmax	(	double	wate,
		double	glift )

References DynamicPressure(), gliftm(), Mach(), pi, and wate.

Referenced by ratmx1().

◆ Position()

virtual UtVec3d & BrawlerMover::Position ( )

inlinevirtual

References pos.

Referenced by Altitude(), aproj3(), and perfrm().

◆ prjacc()

void BrawlerMover::prjacc	(	const UtVec3d &	xin,
		const UtVec3d &	vin,
		const UtVec3d &	a,
		double	dt,
		UtVec3d &	xout,
		UtVec3d &	vout )

Referenced by aproj3().

◆ prlevl()

void BrawlerMover::prlevl	(	double	aGees,
		double	aTurn,
		double	aRoc,
		double	aHeading,
		double	aMach )

References dirct(), forcev(), BRAWLER::headeg(), BRAWLER::ramp(), BRAWLER::sign(), Speed(), and Velocity().

Referenced by CommandLevelTurn().

◆ qmax()

double BrawlerMover::qmax	(	double	u,
		double	wate,
		double	awz,
		const int	idir )

References BRAWLER::amin1(), DynamicPressure(), gcap, gcap2, gliftm(), BRAWLER::grav, Mach(), mchval, miss_mass, BRAWLER::nabort(), nmach1, BRAWLER::tbl1(), and wate.

Referenced by ratmx1().

◆ qroots()

void BrawlerMover::qroots	(	double	a,
		double	b,
		double	c,
		double &	x1,
		double &	x2,
		bool &	solutn )

Referenced by stept().

◆ rates()

void BrawlerMover::rates	(	double &	xl,
		double	thrst,
		double &	dt,
		double	tend,
		UtVec3d &	wact,
		double &	spddes,
		UtVec3d &	vw,
		UtVec3d &	gw,
		UtVec3d &	aw,
		const int	arotyp,
		double &	aoaact,
		double &	aldact )

References actxdt(), aero1, alfa, amass, BRAWLER::amin1(), AngularRates(), aoa(), arotyp, aw, DynamicPressure(), gldmx(), BRAWLER::grav, gwreq(), HEADING_SPEED_ALTITUDE, mAngularRates, mCommandType, mMaxGees, BRAWLER::nabort(), omegp, omegq, pmx, qmxpos, ratmx1(), ReferenceArea(), BRAWLER::sign(), Speed(), VECTOR_GEES, wate, and BRAWLER::xlimit().

Referenced by flyac().

◆ ratmx1()

void BrawlerMover::ratmx1	(	double	xl,
		double	acmass,
		UtVec3d &	avw,
		UtVec3d &	agw,
		double	aoaold,
		double	thrst,
		double &	maxp,
		double &	qmxpos,
		double &	qmxneg,
		double &	aoamx )

References aoamx, aoamx1(), BRAWLER::grav, pmax(), qmax(), qmxpos, and wate.

Referenced by rates().

◆ ReferenceArea()

virtual double BrawlerMover::ReferenceArea ( )

inlinevirtual

References rarea.

Referenced by aoamx1(), Drag(), faoa(), fdrag_inner(), fliftm(), fxlift(), get_aoa(), Lift(), and rates().

◆ rollim()

void BrawlerMover::rollim	(	UtVec3d &	gw,
		double &	roldes,
		double &	aly,
		double &	alz,
		double	psi )

References BRAWLER::grav, ld2, limchk(), mnonrl, mxexrl, over, pi, BRAWLER::rad, rlthrs, rolmx, BRAWLER::sign(), tmacex, tmexrl, tmonrl, tsv, and twopi.

Referenced by gwreq().

◆ RollMax()

virtual double BrawlerMover::RollMax ( )

inlinevirtual

References rolmx.

◆ RollRateMax()

virtual double BrawlerMover::RollRateMax ( )

inlinevirtual

References pmx.

◆ seteng()

void BrawlerMover::seteng	(	double	delt,
		double	drg,
		double	spddes,
		double	tsmn )

References BRAWLER::amax1(), BRAWLER::amin1(), ddpdsv, desaxf(), deseng(), fabsv, fggsv, gas, stenst(), throtm, trpdsv, tset, and ttset.

Referenced by flact1().

◆ SetMaxThrottle()

void BrawlerMover::SetMaxThrottle ( double aThrottle )

References throtm.

Referenced by WsfBrawlerMover::SetMaxThrottle().

◆ spdtoa()

void BrawlerMover::spdtoa	(	double	spd0x,
		double	spdtmp,
		double	dspeed,
		const UtVec3d &	vdes,
		double	dt,
		double	gmax,
		const UtVec3d &	vtemp,
		double &	aldes,
		UtVec3d &	atrans )

References BRAWLER::amax1(), BRAWLER::eps, BRAWLER::grav, and BRAWLER::vorth().

Referenced by aproj3().

◆ SpecificEnergyRate()

virtual double BrawlerMover::SpecificEnergyRate ( )

inlinevirtual

Returns specific energy rate calculated in aproj3.

◆ Speed()

virtual double BrawlerMover::Speed ( )

inlinevirtual

References spd.

Referenced by altlim(), CalibratedAirSpeed(), desaxf(), dirct(), flact1(), flyac(), flyac_short(), forcev(), WsfBrawlerMover::GoToAltitude(), gwreq(), Initialize(), max_asubt(), prlevl(), rates(), WsfBrawlerMover::ReasonableClimbRate(), and WsfBrawlerMover::UpdateRoute().

◆ srch2()

void BrawlerMover::srch2	(	double *	x,
		const int	nx,
		double	xint,
		int &	ilow,
		double &	p )

References BRAWLER::nabort(), and undnum.

Referenced by get_aoa().

◆ State()

UtEntity BrawlerMover::State ( double aSimTime )

virtual

◆ stenst()

void BrawlerMover::stenst	(	double	fggdes,
		double	fabdes,
		double	ddpdes,
		double	trpdes,
		double	delt )

References abdt, BRAWLER::amin1(), ddpdsv, dtggdn, dtggup, fabsv, fggsv, tablim, trefgg, trpdsv, trtd, tset, and ttset.

Referenced by seteng().

◆ stept()

double BrawlerMover::stept	(	double	ades,
		double	w,
		double	angmax,
		double &	wdes,
		double	tau )

References BRAWLER::amax1(), BRAWLER::amin1(), BRAWLER::nabort(), qroots(), BRAWLER::sign(), and stept().

Referenced by gwreq(), and stept().

◆ susgmx()

double BrawlerMover::susgmx	(	double	wate,
		double	thrtlx )

References alpha0, BRAWLER::amax1(), aoamcl(), drag2(), LiftFromAlpha(), BRAWLER::maxcnt(), BRAWLER::sign(), thrust(), and wate.

Referenced by flyac(), and perfrm().

◆ thrdec()

void BrawlerMover::thrdec	(	double	thrtlx,
		double &	fgg,
		double &	fab,
		double &	trpd )

References chkrng(), and throtl.

Referenced by deseng(), effth2(), Thrust(), and thrust().

◆ throt()

double BrawlerMover::throt ( double thrst )

References BRAWLER::amin1(), throt(), throtm, thrust(), tset, and xlo.

Referenced by deseng(), dirct(), and throt().

◆ Throttle()

double BrawlerMover::Throttle ( )

virtual

References tset.

Referenced by WsfBrawlerMover::GetThrottlePosition().

◆ thrst2()

void BrawlerMover::thrst2	(	double	fgg,
		double	fab,
		double &	tgg,
		double &	tab,
		double &	id )

References thrst3().

Referenced by deseng(), and effthr().

◆ thrst3()

void BrawlerMover::thrst3	(	double	fgg,
		double	fab,
		double &	tgg,
		double &	tab,
		double &	id,
		double	trpd,
		bool	destrv )

References chkrng(), fthrst(), BRAWLER::nabort(), trefgg, and undnum.

Referenced by thrst2(), and thrust().

◆ Thrust() [1/2]

virtual double BrawlerMover::Thrust ( double throttle )

inlinevirtual

References InletDrag(), and thrust().

Referenced by WsfBrawlerMover::ReasonableClimbRate().

◆ Thrust() [2/2]

double BrawlerMover::Thrust	(	double	throttle,
		double	speed,
		double	altitude )

virtual

References abcorl, atmos(), gas, htvec, mchval, nhts, nmach1, BRAWLER::tbl2(), thrdec(), thrmx, thrst_adj, tidle, and tmil.

◆ thrust()

void BrawlerMover::thrust	(	double	thrtlx,
		double &	tgg,
		double &	tab,
		double &	id )

References Mach(), thrdec(), thrst3(), and trefgg.

Referenced by allim(), aproj3(), InletDrag(), max_asubt(), perfrm(), WsfBrawlerMover::ReasonableClimbRate(), susgmx(), throt(), and Thrust().

◆ thstoa()

void BrawlerMover::thstoa	(	double	gx,
		double	frclon,
		const UtVec3d &	dir0,
		const UtVec3d &	vtemp,
		double	spdtmp,
		double	dt,
		double	gmax,
		double &	aldes,
		UtVec3d &	atrans )

References amass, amxin, BRAWLER::arccos(), dragvl, BRAWLER::grav, ndatbl, BRAWLER::tbl1b(), and BRAWLER::vorth().

Referenced by aproj3().

◆ toltst()

bool BrawlerMover::toltst	(	double	xf,
		double	x0,
		double	tol )

References chkrng().

Referenced by gwreq().

◆ TurnRadius()

virtual double BrawlerMover::TurnRadius ( )

inlinevirtual

References turn.

Referenced by WsfBrawlerMover::Update().

◆ udrbe()

void BrawlerMover::udrbe	(	UtFortMat3d &	rbe,
		UtVec3d &	w,
		double	wsq,
		double	wmag,
		double	chi )

Referenced by aproj3(), flact1(), flyac_short(), and State().

◆ udxv()

void BrawlerMover::udxv	(	UtVec3d &	accbar,
		UtVec3d &	pos,
		UtVec3d &	vel,
		double	delt,
		UtFortMat3d &	rwea )

References pos, rwea, and vel.

Referenced by flact1().

◆ UpdateFuel()

void BrawlerMover::UpdateFuel	(	double	aTimeStep,
		double	aInitialFlow,
		double	aThrottle,
		double &	aFuelQuantity,
		double &	aVehicleMass )

virtual

Reimplemented in WsfBrawlerMover.

References DeleteMover(), fflo(), and undnum.

Referenced by DeleteMover(), flact1(), and WsfBrawlerMover::UpdateFuel().

◆ UpdateState()

bool BrawlerMover::UpdateState ( double toSimTime )

virtual

References flyac(), and perfrm().

Referenced by operator=(), and WsfBrawlerMover::Update().

◆ Velocity()

virtual UtVec3d & BrawlerMover::Velocity ( )

inlinevirtual

References vel.

Referenced by aproj3(), CommandSlice(), dirct(), flact0(), perfrm(), and prlevl().

◆ VelocityWindAxes()

UtVec3d BrawlerMover::VelocityWindAxes ( void )

virtual

References rwea, and vel.

◆ vmake2()

void BrawlerMover::vmake2	(	double	a,
		UtVec3d &	vin,
		UtVec3d &	vout )

Referenced by altlim().

◆ xlift()

double BrawlerMover::xlift ( double alfa )

References alfa, fxlift(), BRAWLER::nabort(), and undnum.

Referenced by Lift(), and LiftFromAlpha().

Member Data Documentation

◆ abcorl

double BrawlerMover::abcorl

Referenced by BrawlerMover(), BrawlerMover(), fntthr(), LoadAeroConfig(), and Thrust().

◆ abdt

double BrawlerMover::abdt

Referenced by BrawlerMover(), BrawlerMover(), LoadAeroConfig(), and stenst().

◆ ac_acd

double BrawlerMover::ac_acd[2 *max_acd_mach]

Referenced by BrawlerMover(), BrawlerMover(), Drag(), and drag2().

◆ ac_acd_mach

double BrawlerMover::ac_acd_mach[2 *max_acd_mach]

Referenced by BrawlerMover(), BrawlerMover(), Drag(), and drag2().

◆ ac_fuel_cap

double BrawlerMover::ac_fuel_cap

Referenced by BrawlerMover(), BrawlerMover(), and LoadAeroConfig().

◆ acc

UtVec3d BrawlerMover::acc

Referenced by Acceleration(), AccelerationWindAxes(), BrawlerMover(), BrawlerMover(), flact1(), flyac_short(), Initialize(), and State().

◆ aeroLoaded

bool BrawlerMover::aeroLoaded

Referenced by BrawlerMover(), BrawlerMover(), Initialize(), and LoadAeroConfig().

◆ alfa

double BrawlerMover::alfa

Referenced by Alpha(), BrawlerMover(), BrawlerMover(), desaxf(), deseng(), flact1(), flyac(), flyac_short(), fxlift(), gwreq(), Initialize(), rates(), State(), and xlift().

◆ alfdot

double BrawlerMover::alfdot

Referenced by AngleOfAttackRate(), BrawlerMover(), BrawlerMover(), and flyac().

◆ alfv1

double BrawlerMover::alfv1[malpha]

Referenced by aoamcl(), aoamx1(), BrawlerMover(), BrawlerMover(), faoa(), fxlift(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), Lift(), and LoadAeroConfig().

◆ alfv2

double BrawlerMover::alfv2[malpha]

Referenced by BrawlerMover(), BrawlerMover(), CoefficientOfDrag(), get_aoa(), and LoadAeroConfig().

◆ almax

double BrawlerMover::almax

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ almaxg

double BrawlerMover::almaxg

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), and perfrm().

◆ almin

double BrawlerMover::almin

Referenced by BrawlerMover(), BrawlerMover(), max_asubt(), and perfrm().

◆ alming

double BrawlerMover::alming

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ alpha0

double BrawlerMover::alpha0

Referenced by AlphaCL0(), BrawlerMover(), BrawlerMover(), Drag2(), faoa(), fxlift(), Lift(), LoadAeroConfig(), max_asubt(), and susgmx().

◆ altmax

double BrawlerMover::altmax

Referenced by altlim(), BrawlerMover(), and BrawlerMover().

◆ altmin

double BrawlerMover::altmin

Referenced by altlim(), BrawlerMover(), and BrawlerMover().

◆ amass

double BrawlerMover::amass

Referenced by AircraftMass(), aproj3(), BrawlerMover(), BrawlerMover(), desaxf(), deseng(), dirct(), flact1(), flyac(), grthr(), gwreq(), Initialize(), laccel(), max_asubt(), perfrm(), rates(), and thstoa().

◆ amxin

double BrawlerMover::amxin

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), laccel(), perfrm(), and thstoa().

◆ aoa_tab_type

int BrawlerMover::aoa_tab_type

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), faoa(), fxlift(), Lift(), and LoadAeroConfig().

◆ aoamn

double BrawlerMover::aoamn

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ aoamx

double BrawlerMover::aoamx

Referenced by allim(), aoamx1(), BrawlerMover(), BrawlerMover(), laccel(), perfrm(), and ratmx1().

◆ aoavl

double BrawlerMover::aoavl[ndatbl]

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), laccel(), and perfrm().

◆ arotyp

int BrawlerMover::arotyp

Referenced by BrawlerMover(), BrawlerMover(), flyac(), perfrm(), and rates().

◆ aw

UtVec3d BrawlerMover::aw

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandSlice(), flact0(), flyac(), getdt(), gwreq(), manwnd(), perfrm(), and rates().

◆ barems

double BrawlerMover::barems

Referenced by BrawlerMover(), BrawlerMover(), EmptyMass(), flyac(), Initialize(), WsfBrawlerMover::Initialize(), LoadAeroConfig(), and WsfBrawlerMover::Update().

◆ bvrmch

double BrawlerMover::bvrmch

Referenced by BrawlerMover(), BrawlerMover(), CommandSlice(), and Initialize().

◆ casmax

double BrawlerMover::casmax

Referenced by BrawlerMover(), BrawlerMover(), corner(), desaxf(), and LoadAeroConfig().

◆ casmin

double BrawlerMover::casmin

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), and max_asubt().

◆ cdrag

double BrawlerMover::cdrag[mfm *malpha]

Referenced by BrawlerMover(), BrawlerMover(), CoefficientOfDrag(), get_aoa(), and LoadAeroConfig().

◆ clift

double BrawlerMover::clift[mfm *malpha]

Referenced by aoamcl(), aoamx1(), BrawlerMover(), BrawlerMover(), faoa(), fxlift(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), Lift(), and LoadAeroConfig().

◆ clmax

double BrawlerMover::clmax[mfm]

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), corner(), fliftm(), fxlift(), WsfBrawlerProcessor::GetMaxCL(), WsfBrawlerProcessor::GetMaxCL(), WsfBrawlerProcessor::GetMaxCL(), Lift(), and LoadAeroConfig().

◆ cornrv

double BrawlerMover::cornrv

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ crnrv

double BrawlerMover::crnrv

Referenced by BrawlerMover(), BrawlerMover(), and corner().

◆ ddpdsv

double BrawlerMover::ddpdsv

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flacti(), perfrm(), seteng(), and stenst().

◆ densme

double BrawlerMover::densme

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ deswt

double BrawlerMover::deswt

Referenced by BrawlerMover(), BrawlerMover(), and LoadAeroConfig().

◆ dragvl

double BrawlerMover::dragvl[ndatbl]

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), laccel(), perfrm(), and thstoa().

◆ drgaoa

double BrawlerMover::drgaoa[ndtbl2]

Referenced by allim(), BrawlerMover(), BrawlerMover(), and perfrm().

◆ drgnow

double BrawlerMover::drgnow

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ drgsu

double BrawlerMover::drgsu

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ drme

double BrawlerMover::drme

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), getqm(), and perfrm().

◆ dtggdn

double BrawlerMover::dtggdn

Referenced by BrawlerMover(), BrawlerMover(), LoadAeroConfig(), and stenst().

◆ dtggup

double BrawlerMover::dtggup

Referenced by BrawlerMover(), BrawlerMover(), LoadAeroConfig(), and stenst().

◆ dyp

double BrawlerMover::dyp

Referenced by BrawlerMover(), BrawlerMover(), dirct(), DynamicPressure(), flact1(), and Initialize().

◆ epdmax

double BrawlerMover::epdmax

Referenced by BrawlerMover(), BrawlerMover(), grthr(), and perfrm().

◆ epdmin

double BrawlerMover::epdmin

Referenced by BrawlerMover(), BrawlerMover(), grthr(), and perfrm().

◆ epdnow

double BrawlerMover::epdnow

Referenced by BrawlerMover(), BrawlerMover(), grthr(), and perfrm().

◆ fabsv

double BrawlerMover::fabsv

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flacti(), perfrm(), seteng(), and stenst().

◆ ff_adj

double BrawlerMover::ff_adj

Referenced by BrawlerMover(), BrawlerMover(), and fflo().

◆ fggsv

double BrawlerMover::fggsv

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flacti(), perfrm(), seteng(), and stenst().

◆ floidl

double BrawlerMover::floidl[mmach1 *mhts]

Referenced by BrawlerMover(), BrawlerMover(), fflo(), and LoadAeroConfig().

◆ flomax

double BrawlerMover::flomax[mmach1 *mhts]

Referenced by BrawlerMover(), BrawlerMover(), fflo(), and LoadAeroConfig().

◆ flomil

double BrawlerMover::flomil[mmach1 *mhts]

Referenced by BrawlerMover(), BrawlerMover(), fflo(), and LoadAeroConfig().

◆ fm

double BrawlerMover::fm

Referenced by aoamcl(), BrawlerMover(), BrawlerMover(), CommandSlice(), dirct(), flact1(), forcev(), gldmx(), Initialize(), and Mach().

◆ fmmax

double BrawlerMover::fmmax

Referenced by BrawlerMover(), BrawlerMover(), desaxf(), and LoadAeroConfig().

◆ fmvec1

double BrawlerMover::fmvec1[mfm]

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), corner(), fliftm(), fxlift(), WsfBrawlerProcessor::GetMaxCL(), WsfBrawlerProcessor::GetMaxCL(), WsfBrawlerProcessor::GetMaxCL(), Lift(), and LoadAeroConfig().

◆ fmvec2

double BrawlerMover::fmvec2[mfm]

Referenced by aoamcl(), aoamx1(), BrawlerMover(), BrawlerMover(), faoa(), fxlift(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), Lift(), and LoadAeroConfig().

◆ fmvec3

double BrawlerMover::fmvec3[mfm]

Referenced by BrawlerMover(), BrawlerMover(), CoefficientOfDrag(), get_aoa(), and LoadAeroConfig().

◆ gas

double BrawlerMover::gas

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flacti(), flyac(), Gas(), Initialize(), WsfBrawlerMover::Initialize(), LoadAeroConfig(), seteng(), Thrust(), and WsfBrawlerMover::Update().

◆ gcap

double BrawlerMover::gcap[2][mmach1]

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), corner(), WsfBrawlerProcessor::CurrentStructuralGLimit_g(), gldmx(), LoadAeroConfig(), and qmax().

◆ gcap2

double BrawlerMover::gcap2[2][mmach1]

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), corner(), gldmx(), LoadAeroConfig(), qmax(), and WsfBrawlerProcessor::StructuralGLimitAtDesignWeight_g().

◆ gmnin

double BrawlerMover::gmnin

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ gmxin

double BrawlerMover::gmxin

Referenced by BrawlerMover(), BrawlerMover(), flyac(), and perfrm().

◆ gmxsu

double BrawlerMover::gmxsu

Referenced by BrawlerMover(), BrawlerMover(), perfrm(), and WsfBrawlerMover::Update().

◆ gmxsut

double BrawlerMover::gmxsut

Referenced by BrawlerMover(), BrawlerMover(), CommandLevelTurn(), CommandSlice(), forcev(), perfrm(), and WsfBrawlerMover::Update().

◆ gravec

UtVec3d BrawlerMover::gravec

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandSlice(), desaxf(), dirct(), flact0(), GravityWindAxes(), laccel(), max_asubt(), and perfrm().

◆ gwind

UtVec3d BrawlerMover::gwind

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), max_asubt(), and perfrm().

◆ htvec

double BrawlerMover::htvec[mhts]

Referenced by BrawlerMover(), BrawlerMover(), fflo(), fntthr(), LoadAeroConfig(), and Thrust().

◆ ld2

bool BrawlerMover::ld2

Referenced by BrawlerMover(), BrawlerMover(), limchk(), and rollim().

◆ mAltitude

double BrawlerMover::mAltitude

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandHeadingSpeedAltitude(), WsfBrawlerMover::GoToAltitude(), WsfBrawlerMover::GoToLocation(), and gwreq().

◆ mAngularRates

UtVec3d BrawlerMover::mAngularRates

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandRates(), gwreq(), and rates().

◆ mAxialAccel

UtVec3d BrawlerMover::mAxialAccel

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandRates(), desaxf(), flact0(), and gwreq().

◆ mBrawlerPlatformPtr

BrawlerPlatform* BrawlerMover::mBrawlerPlatformPtr

Referenced by BrawlerMover(), BrawlerMover(), Initialize(), WsfBrawlerMover::Initialize(), perfrm(), and WsfBrawlerMover::Update().

◆ mchval

double BrawlerMover::mchval[mmach1]

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), corner(), WsfBrawlerProcessor::CurrentStructuralGLimit_g(), fflo(), fntthr(), gldmx(), LoadAeroConfig(), qmax(), WsfBrawlerProcessor::StructuralGLimitAtDesignWeight_g(), and Thrust().

◆ mCommandType

CommandType BrawlerMover::mCommandType

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandHeadingSpeedAltitude(), CommandPlaneManeuver(), CommandRates(), CommandVector(), desaxf(), flact0(), WsfBrawlerMover::GoToAltitude(), WsfBrawlerMover::GoToLocation(), WsfBrawlerMover::GoToSpeed(), gwreq(), Initialize(), rates(), WsfBrawlerMover::TurnToHeading(), and WsfBrawlerMover::Update().

◆ mHeading

double BrawlerMover::mHeading

Referenced by BrawlerMover(), BrawlerMover(), CommandHeadingSpeedAltitude(), WsfBrawlerMover::GoToLocation(), gwreq(), and WsfBrawlerMover::TurnToHeading().

◆ miss_mass

double BrawlerMover::miss_mass

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), corner(), gldmx(), LoadAeroConfig(), and qmax().

◆ mMaxClimb

double BrawlerMover::mMaxClimb

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandHeadingSpeedAltitude(), WsfBrawlerMover::GoToAltitude(), gwreq(), and WsfBrawlerMover::Update().

◆ mMaxGees

double BrawlerMover::mMaxGees

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandHeadingSpeedAltitude(), CommandPlaneManeuver(), CommandVector(), flact0(), WsfBrawlerMover::GoToSpeed(), gwreq(), Initialize(), rates(), and WsfBrawlerMover::TurnToHeading().

◆ mnonrl

double BrawlerMover::mnonrl

Referenced by BrawlerMover(), BrawlerMover(), and rollim().

◆ mPlane

UtVec3d BrawlerMover::mPlane

Referenced by BrawlerMover(), BrawlerMover(), CommandPlaneManeuver(), and flact0().

◆ mSpeed

double BrawlerMover::mSpeed

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandHeadingSpeedAltitude(), CommandPlaneManeuver(), CommandVector(), WsfBrawlerMover::GoToAltitude(), WsfBrawlerMover::GoToSpeed(), gwreq(), Initialize(), and WsfBrawlerMover::Update().

◆ mThrottle

double BrawlerMover::mThrottle

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandPlaneManeuver(), CommandVector(), and flact1().

◆ mThrottleFlag

bool BrawlerMover::mThrottleFlag

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), CommandHeadingSpeedAltitude(), CommandPlaneManeuver(), CommandVector(), desaxf(), gwreq(), and Initialize().

◆ mVelocityVector

UtVec3d BrawlerMover::mVelocityVector

Referenced by altlim(), aproj3(), BrawlerMover(), BrawlerMover(), CommandVector(), gwreq(), and Initialize().

◆ mxexrl

double BrawlerMover::mxexrl

Referenced by BrawlerMover(), BrawlerMover(), and rollim().

◆ nalph1

int BrawlerMover::nalph1

Referenced by aoamcl(), aoamx1(), BrawlerMover(), BrawlerMover(), faoa(), fxlift(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), Lift(), and LoadAeroConfig().

◆ nalph2

int BrawlerMover::nalph2

Referenced by BrawlerMover(), BrawlerMover(), CoefficientOfDrag(), get_aoa(), and LoadAeroConfig().

◆ nfm1

int BrawlerMover::nfm1

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), corner(), fliftm(), fxlift(), WsfBrawlerProcessor::GetMaxCL(), WsfBrawlerProcessor::GetMaxCL(), WsfBrawlerProcessor::GetMaxCL(), Lift(), and LoadAeroConfig().

◆ nfm2

int BrawlerMover::nfm2

Referenced by aoamcl(), aoamx1(), BrawlerMover(), BrawlerMover(), faoa(), fxlift(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), WsfBrawlerProcessor::GetAlphaAtMaxCL_deg(), Lift(), and LoadAeroConfig().

◆ nfm3

int BrawlerMover::nfm3

Referenced by BrawlerMover(), BrawlerMover(), CoefficientOfDrag(), get_aoa(), and LoadAeroConfig().

◆ nhts

int BrawlerMover::nhts

Referenced by BrawlerMover(), BrawlerMover(), fflo(), fntthr(), LoadAeroConfig(), and Thrust().

◆ nmach1

int BrawlerMover::nmach1

Referenced by aoamx1(), BrawlerMover(), BrawlerMover(), corner(), WsfBrawlerProcessor::CurrentStructuralGLimit_g(), fflo(), fntthr(), gldmx(), LoadAeroConfig(), qmax(), WsfBrawlerProcessor::StructuralGLimitAtDesignWeight_g(), and Thrust().

◆ num_ac_acd_m

int BrawlerMover::num_ac_acd_m

Referenced by BrawlerMover(), BrawlerMover(), Drag(), and drag2().

◆ omegp

double BrawlerMover::omegp

Referenced by BrawlerMover(), BrawlerMover(), gwreq(), LagFilterFreqPitchRate(), and rates().

◆ omegq

double BrawlerMover::omegq

Referenced by BrawlerMover(), BrawlerMover(), gwreq(), LagFilterFreqRollRate(), and rates().

◆ over

bool BrawlerMover::over

Referenced by BrawlerMover(), BrawlerMover(), limchk(), and rollim().

◆ parea

double BrawlerMover::parea[3]

Referenced by BrawlerMover(), BrawlerMover(), and LoadAeroConfig().

◆ pmx

double BrawlerMover::pmx

Referenced by BrawlerMover(), BrawlerMover(), gwreq(), rates(), and RollRateMax().

◆ pos

UtVec3d BrawlerMover::pos

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flyac_short(), Initialize(), Position(), State(), and udxv().

◆ presme

double BrawlerMover::presme

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ prme

double BrawlerMover::prme

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ psubs

double BrawlerMover::psubs

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ qmxpos

double BrawlerMover::qmxpos

Referenced by BrawlerMover(), BrawlerMover(), gwreq(), PitchRatePositiveMax(), rates(), and ratmx1().

◆ radmnp

double BrawlerMover::radmnp

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ rarea

double BrawlerMover::rarea

Referenced by acarea(), BrawlerMover(), BrawlerMover(), LoadAeroConfig(), and ReferenceArea().

◆ rate

double BrawlerMover::rate

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flyac_short(), and State().

◆ rbea

UtFortMat3d BrawlerMover::rbea

Referenced by BrawlerMover(), BrawlerMover(), EarthToBodyRotationMatrix(), flact1(), flyac_short(), and Initialize().

◆ rfarea

double BrawlerMover::rfarea[msweep]

Referenced by acarea(), BrawlerMover(), BrawlerMover(), and LoadAeroConfig().

◆ rlthrs

double BrawlerMover::rlthrs

Referenced by BrawlerMover(), BrawlerMover(), and rollim().

◆ rolmx

double BrawlerMover::rolmx

Referenced by BrawlerMover(), BrawlerMover(), rollim(), and RollMax().

◆ rwea

UtFortMat3d BrawlerMover::rwea

Referenced by AccelerationWindAxes(), adjal(), altlim(), BrawlerMover(), BrawlerMover(), desaxf(), EarthToWindRotationMatrix(), flact1(), flyac_short(), GravityWindAxes(), gwreq(), Initialize(), max_asubt(), State(), udxv(), and VelocityWindAxes().

◆ spd

double BrawlerMover::spd

Referenced by BrawlerMover(), BrawlerMover(), corner(), flact1(), flyac_short(), forcev(), Initialize(), laccel(), and Speed().

◆ svtime

double BrawlerMover::svtime

Referenced by BrawlerMover(), and BrawlerMover().

◆ tablim

bool BrawlerMover::tablim

Referenced by BrawlerMover(), BrawlerMover(), LoadAeroConfig(), and stenst().

◆ tdlim

bool BrawlerMover::tdlim

Referenced by BrawlerMover(), BrawlerMover(), desaxf(), and LoadAeroConfig().

◆ tempme

double BrawlerMover::tempme

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ thrmax

double BrawlerMover::thrmax

Referenced by BrawlerMover(), BrawlerMover(), grthr(), laccel(), and perfrm().

◆ thrmin

double BrawlerMover::thrmin

Referenced by BrawlerMover(), BrawlerMover(), grthr(), and perfrm().

◆ thrmx

double BrawlerMover::thrmx[mmach1 *mhts]

Referenced by BrawlerMover(), BrawlerMover(), fntthr(), LoadAeroConfig(), and Thrust().

◆ thrnow

double BrawlerMover::thrnow

Referenced by BrawlerMover(), BrawlerMover(), grthr(), and perfrm().

◆ throtl

double BrawlerMover::throtl

Referenced by BrawlerMover(), BrawlerMover(), and thrdec().

◆ throtm

double BrawlerMover::throtm

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), effthr(), fflo(), gwreq(), max_asubt(), MaxAllowedThrottle(), perfrm(), seteng(), SetMaxThrottle(), and throt().

◆ thrst_adj

double BrawlerMover::thrst_adj

Referenced by BrawlerMover(), BrawlerMover(), fntthr(), and Thrust().

◆ thrstl

double BrawlerMover::thrstl[5]

Referenced by aproj3(), BrawlerMover(), BrawlerMover(), and perfrm().

◆ tidle

double BrawlerMover::tidle[mmach1 *mhts]

Referenced by BrawlerMover(), BrawlerMover(), fntthr(), LoadAeroConfig(), and Thrust().

◆ tmacex

double BrawlerMover::tmacex

Referenced by BrawlerMover(), BrawlerMover(), and rollim().

◆ tmexrl

double BrawlerMover::tmexrl

Referenced by BrawlerMover(), BrawlerMover(), and rollim().

◆ tmil

double BrawlerMover::tmil[mmach1 *mhts]

Referenced by BrawlerMover(), BrawlerMover(), fntthr(), LoadAeroConfig(), and Thrust().

◆ tmlim

bool BrawlerMover::tmlim

Referenced by BrawlerMover(), BrawlerMover(), deseng(), and LoadAeroConfig().

◆ tmonrl

double BrawlerMover::tmonrl

Referenced by BrawlerMover(), BrawlerMover(), and rollim().

◆ trefgg

double BrawlerMover::trefgg

Referenced by BrawlerMover(), BrawlerMover(), desaxf(), deseng(), effthr(), LoadAeroConfig(), stenst(), thrst3(), and thrust().

◆ trmla

double BrawlerMover::trmla

Referenced by BrawlerMover(), BrawlerMover(), desaxf(), and LoadAeroConfig().

◆ trmm

double BrawlerMover::trmm

Referenced by BrawlerMover(), BrawlerMover(), deseng(), and LoadAeroConfig().

◆ trpdsv

double BrawlerMover::trpdsv

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flacti(), perfrm(), seteng(), and stenst().

◆ trtd

double BrawlerMover::trtd

Referenced by BrawlerMover(), BrawlerMover(), LoadAeroConfig(), and stenst().

◆ tset

double BrawlerMover::tset

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flacti(), seteng(), stenst(), throt(), and Throttle().

◆ tsv

double BrawlerMover::tsv

Referenced by BrawlerMover(), BrawlerMover(), flyac(), Initialize(), PlatformTime(), rollim(), State(), WsfBrawlerMover::SwapMoverInitiated(), WsfBrawlerMover::TurnOn(), and WsfBrawlerMover::Update().

◆ ttset

double BrawlerMover::ttset

Referenced by BrawlerMover(), BrawlerMover(), seteng(), and stenst().

◆ turn

double BrawlerMover::turn

Referenced by BrawlerMover(), BrawlerMover(), flyac(), and TurnRadius().

◆ vel

UtVec3d BrawlerMover::vel

Referenced by adjal(), altlim(), BrawlerMover(), BrawlerMover(), flact1(), flyac_short(), gwreq(), Initialize(), State(), udxv(), Velocity(), and VelocityWindAxes().

◆ vsme

double BrawlerMover::vsme

Referenced by BrawlerMover(), BrawlerMover(), getqm(), and perfrm().

◆ wate

double BrawlerMover::wate

Referenced by aoamcl(), aoamx1(), BrawlerMover(), BrawlerMover(), corner(), flact1(), fliftm(), flyac(), gldmx(), gliftm(), WsfBrawlerProcessor::MaxInstantaneousGLoad_g(), perfrm(), pmax(), qmax(), rates(), ratmx1(), and susgmx().

◆ wmax

double BrawlerMover::wmax

Referenced by BrawlerMover(), BrawlerMover(), and perfrm().

◆ wnow

UtVec3d BrawlerMover::wnow

Referenced by AngularRates(), BrawlerMover(), BrawlerMover(), desang(), flact1(), and getdt().

◆ wsqr

double BrawlerMover::wsqr

Referenced by BrawlerMover(), BrawlerMover(), flact1(), flyac_short(), and State().

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

Public Types

Public Member Functions

Public Attributes

Protected Member Functions

Member Enumeration Documentation

◆ CommandType

Constructor & Destructor Documentation

◆ BrawlerMover() [1/2]

◆ BrawlerMover() [2/2]

◆ ~BrawlerMover()

Member Function Documentation

◆ acarea()

◆ Acceleration()

◆ AccelerationWindAxes()

◆ actxdt()

◆ adjal()

◆ AircraftMass()

◆ allim()

◆ Alpha()

◆ AlphaCL0()

◆ Altitude()

◆ altlim()

◆ AngleOfAttackFromDrag()

◆ AngleOfAttackFromLift()

◆ AngleOfAttackRate()

◆ AngularRates()

◆ aoa()

◆ aoamcl()

◆ aoamx1()

◆ aproj3()

◆ atmos()

◆ AxialForceX()

◆ CalibratedAirSpeed()

◆ cas()

◆ chkrng()

◆ ckrngi()

◆ CoefficientOfDrag()

◆ CoefficientOfLift()

◆ CommandHeadingSpeedAltitude()

◆ CommandLevelTurn()

◆ CommandPlaneManeuver()

◆ CommandRates()

◆ CommandSlice()

◆ CommandVector()

◆ corner()

◆ DeleteMover()

◆ desang()

◆ desaxf()

◆ deseng()

◆ dirct()

◆ Drag()

◆ drag()

◆ Drag2()

◆ drag2()

◆ drgad()

◆ dsxdot()

◆ DynamicPressure()

◆ EarthToBodyRotationMatrix()

◆ EarthToWindRotationMatrix()

◆ effth2()

◆ effthr()

◆ EmptyMass()

◆ faoa()

◆ fdrag2()

◆ fdrag_inner()

◆ fflo()

◆ flact0()

◆ flact1()

◆ flacti()

◆ fliftm()

◆ flyac()

◆ flyac_short()

◆ fntthr()

◆ forcev()

◆ fthrst()

◆ fxlift()

◆ Gas()

◆ gcdadd()

◆ get_aoa()

◆ getdt()