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

Detailed Description

The trimming routine for JSBSim.

FGTrim finds the aircraft attitude and control settings needed to maintain the steady state described by the FGInitialCondition object . It does this iteratively by assigning a control to each state and adjusting that control until the state is within a specified tolerance of zero. States include the recti-linear accelerations udot, vdot, and wdot, the angular accelerations qdot, pdot, and rdot, and the difference between heading and ground track. Controls include the usual flight deck controls available to the pilot plus angle of attack (alpha), sideslip angle(beta), flight path angle (gamma), pitch attitude(theta), roll attitude(phi), and altitude above ground. The last three are used for on-ground trimming. The state-control pairs used in a given trim are completely user configurable and several pre-defined modes are provided as well. They are:

  • tLongitudinal: Trim wdot with alpha, udot with thrust, qdot with elevator
  • tFull: tLongitudinal + vdot with phi, pdot with aileron, rdot with rudder and heading minus ground track (hmgt) with beta
  • tPullup: tLongitudinal but adjust alpha to achieve load factor input with SetTargetNlf()
  • tGround: wdot with altitude, qdot with theta, and pdot with phi

The remaining modes include tCustom, which is completely user defined and tNone.

Note that trims can (and do) fail for reasons that are completely outside the control of the trimming routine itself. The most common problem is the initial conditions: is the model capable of steady state flight at those conditions? Check the speed, altitude, configuration (flaps, gear, etc.), weight, cg, and anything else that may be relevant.

Example usage:

FGFDMExec* FDMExec = new FGFDMExec();
FGInitialCondition* fgic = new FGInitialCondition(FDMExec);
FGTrim fgt(FDMExec, fgic, tFull);
fgic->SetVcaibratedKtsIC(100);
fgic->SetAltitudeFtIC(1000);
fgic->SetClimbRate(500);
if( !fgt.DoTrim() ) {
cout << "Trim Failed" << endl;
}
fgt.Report();
Author
Tony Peden

Definition at line 123 of file FGTrim.h.

#include <FGTrim.h>

+ Inheritance diagram for FGTrim:
+ Collaboration diagram for FGTrim:

Public Member Functions

 FGTrim (FGFDMExec *FDMExec, TrimMode tm=tGround)
 Initializes the trimming class. More...
 
bool AddState (State state, Control control)
 Add a state-control pair to the current configuration. More...
 
void ClearDebug (void)
 
void ClearStates (void)
 Clear all state-control pairs from the current configuration. More...
 
void DebugState (State state)
 Output debug data for one of the axes The State enum is defined in FGTrimAxis.h.
 
bool DoTrim (void)
 Execute the trim.
 
bool EditState (State state, Control new_control)
 Change the control used to zero a state previously configured. More...
 
bool GetGammaFallback (void)
 query the fallback state More...
 
double GetTargetNlf (void)
 
bool RemoveState (State state)
 Remove a specific state-control pair from the current configuration. More...
 
void Report (void)
 Print the results of the trim. More...
 
void SetDebug (int level)
 Debug level 1 shows results of each top-level iteration Debug level 2 shows level 1 & results of each per-axis iteration.
 
void SetGammaFallback (bool bb)
 automatically switch to trimming longitudinal acceleration with flight path angle (gamma) once it becomes apparent that there is not enough/too much thrust. More...
 
void SetMaxCycles (int ii)
 Set the iteration limit. More...
 
void SetMaxCyclesPerAxis (int ii)
 Set the per-axis iteration limit. More...
 
void SetMode (TrimMode tm)
 Clear all state-control pairs and set a predefined trim mode. More...
 
void SetTargetNlf (double nlf)
 
void SetTolerance (double tt)
 Set the tolerance for declaring a state trimmed. More...
 
void TrimStats ()
 Iteration statistics.
 
- 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

◆ FGTrim()

FGTrim ( FGFDMExec FDMExec,
TrimMode  tm = tGround 
)

Initializes the trimming class.

Parameters
FDMExecpointer to a JSBSim executive object.
tmtrim mode

Definition at line 61 of file FGTrim.cpp.

62  : fgic(FDMExec)
63 {
64 
65  Nsub=0;
66  max_iterations=60;
67  max_sub_iterations=100;
68  Tolerance=1E-3;
69  A_Tolerance = Tolerance / 10;
70 
71  Debug=0;DebugLevel=0;
72  fdmex=FDMExec;
73  fgic = *fdmex->GetIC();
74  total_its=0;
75  gamma_fallback=false;
76  mode=tt;
77  xlo=xhi=alo=ahi=0.0;
78  targetNlf=fgic.GetTargetNlfIC();
79  debug_axis=tAll;
80  SetMode(tt);
81  if (debug_lvl & 2) cout << "Instantiated: FGTrim" << endl;
82 }
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Member Function Documentation

◆ AddState()

bool AddState ( State  state,
Control  control 
)

Add a state-control pair to the current configuration.

See the enums State and Control in FGTrimAxis.h for the available options. Will fail if the given state is already configured.

Parameters
statethe accel or other condition to zero
controlthe control used to zero the state
Returns
true if add is successful

Definition at line 130 of file FGTrim.cpp.

130  {
131  mode = tCustom;
132  vector <FGTrimAxis>::iterator iAxes = TrimAxes.begin();
133  for (; iAxes != TrimAxes.end(); ++iAxes) {
134  if (iAxes->GetStateType() == state)
135  return false;
136  }
137 
138  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,state,control));
139  sub_iterations.resize(TrimAxes.size());
140  successful.resize(TrimAxes.size());
141  solution.resize(TrimAxes.size());
142 
143  return true;
144 }

◆ ClearStates()

void ClearStates ( void  )

Clear all state-control pairs from the current configuration.

The trimming routine must have at least one state-control pair configured to be useful

Definition at line 122 of file FGTrim.cpp.

122  {
123  mode=tCustom;
124  TrimAxes.clear();
125  //cout << "TrimAxes.size(): " << TrimAxes.size() << endl;
126 }
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◆ EditState()

bool EditState ( State  state,
Control  new_control 
)

Change the control used to zero a state previously configured.

Parameters
statethe accel or other condition to zero
new_controlthe control used to zero the state

Definition at line 171 of file FGTrim.cpp.

171  {
172  mode = tCustom;
173  vector <FGTrimAxis>::iterator iAxes = TrimAxes.begin();
174  while (iAxes != TrimAxes.end()) {
175  if( iAxes->GetStateType() == state ) {
176  *iAxes = FGTrimAxis(fdmex,&fgic,state,new_control);
177  return true;
178  }
179  ++iAxes;
180  }
181  return false;
182 }

◆ GetGammaFallback()

bool GetGammaFallback ( void  )
inline

query the fallback state

Returns
true if fallback is enabled.

Definition at line 249 of file FGTrim.h.

249 { return gamma_fallback; }

◆ RemoveState()

bool RemoveState ( State  state)

Remove a specific state-control pair from the current configuration.

Parameters
statethe state to remove
Returns
true if removal is successful

Definition at line 148 of file FGTrim.cpp.

148  {
149  bool result=false;
150 
151  mode = tCustom;
152  vector <FGTrimAxis>::iterator iAxes = TrimAxes.begin();
153  while (iAxes != TrimAxes.end()) {
154  if( iAxes->GetStateType() == state ) {
155  iAxes = TrimAxes.erase(iAxes);
156  result=true;
157  continue;
158  }
159  ++iAxes;
160  }
161  if(result) {
162  sub_iterations.resize(TrimAxes.size());
163  successful.resize(TrimAxes.size());
164  solution.resize(TrimAxes.size());
165  }
166  return result;
167 }

◆ Report()

void Report ( void  )

Print the results of the trim.

For each axis trimmed, this includes the final state value, control value, and tolerance used.

Returns
true if trim succeeds

Definition at line 113 of file FGTrim.cpp.

113  {
114  cout << " Trim Results: " << endl;
115  for(unsigned int current_axis=0; current_axis<TrimAxes.size(); current_axis++)
116  TrimAxes[current_axis].AxisReport();
117 
118 }

◆ SetGammaFallback()

void SetGammaFallback ( bool  bb)
inline

automatically switch to trimming longitudinal acceleration with flight path angle (gamma) once it becomes apparent that there is not enough/too much thrust.

Parameters
bbtrue to enable fallback

Definition at line 244 of file FGTrim.h.

244 { gamma_fallback=bb; }

◆ SetMaxCycles()

void SetMaxCycles ( int  ii)
inline

Set the iteration limit.

DoTrim() will return false if limit iterations are reached before trim is achieved. The default is 60. This does not ordinarily need to be changed.

Parameters
iiinteger iteration limit

Definition at line 256 of file FGTrim.h.

256 { max_iterations = ii; }

◆ SetMaxCyclesPerAxis()

void SetMaxCyclesPerAxis ( int  ii)
inline

Set the per-axis iteration limit.

Attempt to zero each state by iterating limit times before moving on to the next. The default limit is 100 and also does not ordinarily need to be changed.

Parameters
iiinteger iteration limit

Definition at line 264 of file FGTrim.h.

264 { max_sub_iterations = ii; }

◆ SetMode()

void SetMode ( TrimMode  tm)

Clear all state-control pairs and set a predefined trim mode.

Parameters
tmthe set of axes to trim. Can be: tLongitudinal, tFull, tGround, tCustom, or tNone

Definition at line 800 of file FGTrim.cpp.

800  {
801  ClearStates();
802  mode=tt;
803  switch(tt) {
804  case tFull:
805  if (debug_lvl > 0)
806  cout << " Full Trim" << endl;
807  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tWdot,tAlpha));
808  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tUdot,tThrottle ));
809  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tQdot,tPitchTrim ));
810  //TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tHmgt,tBeta ));
811  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tVdot,tPhi ));
812  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tPdot,tAileron ));
813  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tRdot,tRudder ));
814  break;
815  case tLongitudinal:
816  if (debug_lvl > 0)
817  cout << " Longitudinal Trim" << endl;
818  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tWdot,tAlpha ));
819  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tUdot,tThrottle ));
820  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tQdot,tPitchTrim ));
821  break;
822  case tGround:
823  if (debug_lvl > 0)
824  cout << " Ground Trim" << endl;
825  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tWdot,tAltAGL ));
826  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tQdot,tTheta ));
827  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tPdot,tPhi ));
828  break;
829  case tPullup:
830  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tNlf,tAlpha ));
831  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tUdot,tThrottle ));
832  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tQdot,tPitchTrim ));
833  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tHmgt,tBeta ));
834  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tVdot,tPhi ));
835  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tPdot,tAileron ));
836  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tRdot,tRudder ));
837  break;
838  case tTurn:
839  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tWdot,tAlpha ));
840  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tUdot,tThrottle ));
841  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tQdot,tPitchTrim ));
842  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tVdot,tBeta ));
843  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tPdot,tAileron ));
844  TrimAxes.push_back(FGTrimAxis(fdmex,&fgic,tRdot,tRudder ));
845  break;
846  case tCustom:
847  case tNone:
848  break;
849  }
850  //cout << "TrimAxes.size(): " << TrimAxes.size() << endl;
851  sub_iterations.resize(TrimAxes.size());
852  successful.resize(TrimAxes.size());
853  solution.resize(TrimAxes.size());
854 }
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◆ SetTolerance()

void SetTolerance ( double  tt)
inline

Set the tolerance for declaring a state trimmed.

Angular accels are held to a tolerance of 1/10th of the given. The default is 0.001 for the recti-linear accelerations and 0.0001 for the angular.

Definition at line 270 of file FGTrim.h.

270  {
271  Tolerance = tt;
272  A_Tolerance = tt / 10;
273  }

The documentation for this class was generated from the following files:
JSBSim::FGTrim::ClearStates
void ClearStates(void)
Clear all state-control pairs from the current configuration.
Definition: FGTrim.cpp:122
JSBSim::FGFDMExec::GetIC
FGInitialCondition * GetIC(void)
Returns a pointer to the FGInitialCondition object.
Definition: FGFDMExec.h:387
JSBSim::FGTrim::FGTrim
FGTrim(FGFDMExec *FDMExec, TrimMode tm=tGround)
Initializes the trimming class.
Definition: FGTrim.cpp:61
JSBSim::FGTrim::SetMode
void SetMode(TrimMode tm)
Clear all state-control pairs and set a predefined trim mode.
Definition: FGTrim.cpp:800
JSBSim::FGInitialCondition::GetTargetNlfIC
double GetTargetNlfIC(void) const
Gets the target normal load factor set from IC.
Definition: FGInitialCondition.h:668