JSBSim Flight Dynamics Model  1.1.11 (13 Feb 2022)
An Open Source Flight Dynamics and Control Software Library in C++
FGTrimAxis Class Reference

Detailed Description

Definition at line 87 of file FGTrimAxis.h.

+ Inheritance diagram for FGTrimAxis:
+ Collaboration diagram for FGTrimAxis:

Public Member Functions

 FGTrimAxis (FGFDMExec *fdmex, FGInitialCondition *IC, State state, Control control)
 Constructor for Trim Axis class. More...
 
 ~FGTrimAxis ()
 Destructor.
 
void AxisReport (void)
 
double GetAvgStability (void)
 
double GetControl (void)
 
double GetControlMax (void)
 
double GetControlMin (void)
 
std::string GetControlName (void)
 
Control GetControlType (void)
 
int GetIterationLimit (void)
 
int GetRunCount (void)
 
double GetSolverEps (void)
 
int GetStability (void)
 
double GetState (void)
 
std::string GetStateName (void)
 
double GetStateTarget (void)
 
State GetStateType (void)
 
double GetTolerance (void)
 
bool InTolerance (void)
 
void Run (void)
 This function iterates through a call to the FGFDMExec::RunIC() function until the desired trimming condition falls inside a tolerance.
 
void SetControl (double value)
 
void SetControlLimits (double min, double max)
 
void SetControlToMax (void)
 
void SetControlToMin (void)
 
void SetIterationLimit (int ii)
 
void SetSolverEps (double ff)
 
void SetStateTarget (double target)
 
void SetTolerance (double ff)
 
- Public Member Functions inherited from FGJSBBase
 FGJSBBase ()
 Constructor for FGJSBBase.
 
virtual ~FGJSBBase ()
 Destructor for FGJSBBase.
 
void PutMessage (const Message &msg)
 Places a Message structure on the Message queue. More...
 
void PutMessage (const std::string &text)
 Creates a message with the given text and places it on the queue. More...
 
void PutMessage (const std::string &text, bool bVal)
 Creates a message with the given text and boolean value and places it on the queue. More...
 
void PutMessage (const std::string &text, int iVal)
 Creates a message with the given text and integer value and places it on the queue. More...
 
void PutMessage (const std::string &text, double dVal)
 Creates a message with the given text and double value and places it on the queue. More...
 
int SomeMessages (void) const
 Reads the message on the queue (but does not delete it). More...
 
void ProcessMessage (void)
 Reads the message on the queue and removes it from the queue. More...
 
MessageProcessNextMessage (void)
 Reads the next message on the queue and removes it from the queue. More...
 
void disableHighLighting (void)
 Disables highlighting in the console output.
 

Additional Inherited Members

- Public Types inherited from FGJSBBase
enum  { eL = 1, eM, eN }
 Moments L, M, N.
 
enum  { eP = 1, eQ, eR }
 Rates P, Q, R.
 
enum  { eU = 1, eV, eW }
 Velocities U, V, W.
 
enum  { eX = 1, eY, eZ }
 Positions X, Y, Z.
 
enum  { ePhi = 1, eTht, ePsi }
 Euler angles Phi, Theta, Psi.
 
enum  { eDrag = 1, eSide, eLift }
 Stability axis forces, Drag, Side force, Lift.
 
enum  { eRoll = 1, ePitch, eYaw }
 Local frame orientation Roll, Pitch, Yaw.
 
enum  { eNorth = 1, eEast, eDown }
 Local frame position North, East, Down.
 
enum  { eLat = 1, eLong, eRad }
 Locations Radius, Latitude, Longitude.
 
enum  {
  inNone = 0, inDegrees, inRadians, inMeters,
  inFeet
}
 Conversion specifiers.
 
- Static Public Member Functions inherited from FGJSBBase
static const std::string & GetVersion (void)
 Returns the version number of JSBSim. More...
 
static constexpr double KelvinToFahrenheit (double kelvin)
 Converts from degrees Kelvin to degrees Fahrenheit. More...
 
static constexpr double CelsiusToRankine (double celsius)
 Converts from degrees Celsius to degrees Rankine. More...
 
static constexpr double RankineToCelsius (double rankine)
 Converts from degrees Rankine to degrees Celsius. More...
 
static constexpr double KelvinToRankine (double kelvin)
 Converts from degrees Kelvin to degrees Rankine. More...
 
static constexpr double RankineToKelvin (double rankine)
 Converts from degrees Rankine to degrees Kelvin. More...
 
static constexpr double FahrenheitToCelsius (double fahrenheit)
 Converts from degrees Fahrenheit to degrees Celsius. More...
 
static constexpr double CelsiusToFahrenheit (double celsius)
 Converts from degrees Celsius to degrees Fahrenheit. More...
 
static constexpr double CelsiusToKelvin (double celsius)
 Converts from degrees Celsius to degrees Kelvin. More...
 
static constexpr double KelvinToCelsius (double kelvin)
 Converts from degrees Kelvin to degrees Celsius. More...
 
static constexpr double FeetToMeters (double measure)
 Converts from feet to meters. More...
 
static double PitotTotalPressure (double mach, double p)
 Compute the total pressure in front of the Pitot tube. More...
 
static double MachFromImpactPressure (double qc, double p)
 Compute the Mach number from the differential pressure (qc) and the static pressure. More...
 
static double VcalibratedFromMach (double mach, double p)
 Calculate the calibrated airspeed from the Mach number. More...
 
static double MachFromVcalibrated (double vcas, double p)
 Calculate the Mach number from the calibrated airspeed.Based on the formulas in the US Air Force Aircraft Performance Flight Testing Manual (AFFTC-TIH-99-01). More...
 
static bool EqualToRoundoff (double a, double b)
 Finite precision comparison. More...
 
static bool EqualToRoundoff (float a, float b)
 Finite precision comparison. More...
 
static bool EqualToRoundoff (float a, double b)
 Finite precision comparison. More...
 
static bool EqualToRoundoff (double a, float b)
 Finite precision comparison. More...
 
static constexpr double Constrain (double min, double value, double max)
 Constrain a value between a minimum and a maximum value.
 
static constexpr double sign (double num)
 
static double GaussianRandomNumber (void)
 
- Static Public Attributes inherited from FGJSBBase
static char highint [5] = {27, '[', '1', 'm', '\0' }
 highlights text
 
static char halfint [5] = {27, '[', '2', 'm', '\0' }
 low intensity text
 
static char normint [6] = {27, '[', '2', '2', 'm', '\0' }
 normal intensity text
 
static char reset [5] = {27, '[', '0', 'm', '\0' }
 resets text properties
 
static char underon [5] = {27, '[', '4', 'm', '\0' }
 underlines text
 
static char underoff [6] = {27, '[', '2', '4', 'm', '\0' }
 underline off
 
static char fgblue [6] = {27, '[', '3', '4', 'm', '\0' }
 blue text
 
static char fgcyan [6] = {27, '[', '3', '6', 'm', '\0' }
 cyan text
 
static char fgred [6] = {27, '[', '3', '1', 'm', '\0' }
 red text
 
static char fggreen [6] = {27, '[', '3', '2', 'm', '\0' }
 green text
 
static char fgdef [6] = {27, '[', '3', '9', 'm', '\0' }
 default text
 
static short debug_lvl = 1
 
- Static Protected Member Functions inherited from FGJSBBase
static std::string CreateIndexedPropertyName (const std::string &Property, int index)
 
- Static Protected Attributes inherited from FGJSBBase
static Message localMsg
 
static std::queue< MessageMessages
 
static unsigned int messageId = 0
 
static constexpr double radtodeg = 180. / M_PI
 
static constexpr double degtorad = M_PI / 180.
 
static constexpr double hptoftlbssec = 550.0
 
static constexpr double psftoinhg = 0.014138
 
static constexpr double psftopa = 47.88
 
static constexpr double ktstofps = 1.68781
 
static constexpr double fpstokts = 1.0 / ktstofps
 
static constexpr double inchtoft = 1.0/12.0
 
static constexpr double fttom = 0.3048
 
static constexpr double m3toft3 = 1.0/(fttom*fttom*fttom)
 
static constexpr double in3tom3 = inchtoft*inchtoft*inchtoft/m3toft3
 
static constexpr double inhgtopa = 3386.38
 
static constexpr double slugtolb = 32.174049
 Note that definition of lbtoslug by the inverse of slugtolb and not to a different constant you can also get from some tables will make lbtoslug*slugtolb == 1 up to the magnitude of roundoff. More...
 
static constexpr double lbtoslug = 1.0/slugtolb
 
static constexpr double kgtolb = 2.20462
 
static constexpr double kgtoslug = 0.06852168
 
static const std::string needed_cfg_version = "2.0"
 
static const std::string JSBSim_version = JSBSIM_VERSION " " __DATE__ " " __TIME__
 
static int gaussian_random_number_phase = 0
 

Constructor & Destructor Documentation

◆ FGTrimAxis()

FGTrimAxis ( FGFDMExec fdmex,
FGInitialCondition IC,
State  state,
Control  control 
)

Constructor for Trim Axis class.

Parameters
fdmexFGFDMExec pointer
ICpointer to initial conditions instance
statea State type (enum)
controla Control type (enum)

Definition at line 61 of file FGTrimAxis.cpp.

62  {
63 
64  fdmex=fdex;
65  fgic=ic;
66  state=st;
67  control=ctrl;
68  max_iterations=10;
69  control_value=0;
70  its_to_stable_value=0;
71  total_iterations=0;
72  total_stability_iterations=0;
73  state_convert=1.0;
74  control_convert=1.0;
75  state_value=0;
76  state_target=0;
77  switch(state) {
78  case tUdot: tolerance = DEFAULT_TOLERANCE; break;
79  case tVdot: tolerance = DEFAULT_TOLERANCE; break;
80  case tWdot: tolerance = DEFAULT_TOLERANCE; break;
81  case tQdot: tolerance = DEFAULT_TOLERANCE / 10; break;
82  case tPdot: tolerance = DEFAULT_TOLERANCE / 10; break;
83  case tRdot: tolerance = DEFAULT_TOLERANCE / 10; break;
84  case tHmgt: tolerance = 0.01; break;
85  case tNlf: state_target=1.0; tolerance = 1E-5; break;
86  case tAll: break;
87  }
88 
89  solver_eps=tolerance;
90  switch(control) {
91  case tThrottle:
92  control_min=0;
93  control_max=1;
94  control_value=0.5;
95  break;
96  case tBeta:
97  control_min=-30*degtorad;
98  control_max=30*degtorad;
99  control_convert=radtodeg;
100  break;
101  case tAlpha:
102  control_min=fdmex->GetAerodynamics()->GetAlphaCLMin();
103  control_max=fdmex->GetAerodynamics()->GetAlphaCLMax();
104  if(control_max <= control_min) {
105  control_max=20*degtorad;
106  control_min=-5*degtorad;
107  }
108  control_value= (control_min+control_max)/2;
109  control_convert=radtodeg;
110  solver_eps=tolerance/100;
111  break;
112  case tPitchTrim:
113  case tElevator:
114  case tRollTrim:
115  case tAileron:
116  case tYawTrim:
117  case tRudder:
118  control_min=-1;
119  control_max=1;
120  state_convert=radtodeg;
121  solver_eps=tolerance/100;
122  break;
123  case tAltAGL:
124  control_min=0;
125  control_max=30;
126  control_value=ic->GetAltitudeAGLFtIC();
127  solver_eps=tolerance/100;
128  break;
129  case tTheta:
130  control_min=ic->GetThetaRadIC() - 5*degtorad;
131  control_max=ic->GetThetaRadIC() + 5*degtorad;
132  state_convert=radtodeg;
133  break;
134  case tPhi:
135  control_min=ic->GetPhiRadIC() - 30*degtorad;
136  control_max=ic->GetPhiRadIC() + 30*degtorad;
137  state_convert=radtodeg;
138  control_convert=radtodeg;
139  break;
140  case tGamma:
141  solver_eps=tolerance/100;
142  control_min=-80*degtorad;
143  control_max=80*degtorad;
144  control_convert=radtodeg;
145  break;
146  case tHeading:
147  control_min=ic->GetPsiRadIC() - 30*degtorad;
148  control_max=ic->GetPsiRadIC() + 30*degtorad;
149  state_convert=radtodeg;
150  break;
151  }
152 
153 
154  Debug(0);
155 }
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The documentation for this class was generated from the following files:
JSBSim::FGFDMExec::GetAerodynamics
FGAerodynamics * GetAerodynamics(void)
Returns the FGAerodynamics pointer.
Definition: FGFDMExec.h:365