![]() |
JSBSim Flight Dynamics Model
1.0 (02 March 2017)
An Open Source Flight Dynamics and Control Software Library in C++
|
Encapsulates a Accelerometer component for the flight control system. More...
#include <FGAccelerometer.h>
Public Member Functions | |
FGAccelerometer (FGFCS *fcs, Element *element) | |
bool | Run (void) |
![]() | |
FGSensor (FGFCS *fcs, Element *element) | |
double | GetFailHigh (void) const |
double | GetFailLow (void) const |
double | GetFailStuck (void) const |
int | GetQuantized (void) const |
void | ResetPastStates (void) |
void | SetFailHigh (double val) |
void | SetFailLow (double val) |
void | SetFailStuck (double val) |
![]() | |
FGFCSComponent (FGFCS *fcs, Element *el) | |
Constructor. | |
virtual | ~FGFCSComponent () |
Destructor. | |
std::string | GetName (void) const |
double | GetOutput (void) const |
virtual double | GetOutputPct (void) const |
std::string | GetType (void) const |
void | SetDtForFrameCount (int FrameCount) |
virtual void | SetOutput (void) |
![]() | |
FGJSBBase () | |
Constructor for FGJSBBase. | |
virtual | ~FGJSBBase () |
Destructor for FGJSBBase. | |
void | disableHighLighting (void) |
Disables highlighting in the console output. | |
std::string | GetVersion (void) |
Returns the version number of JSBSim. More... | |
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) |
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... | |
Message * | ProcessNextMessage (void) |
Reads the next message on the queue and removes it from the queue. More... | |
![]() | |
FGSensorOrientation (Element *element) | |
Additional Inherited Members | |
![]() | |
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 double | CelsiusToFahrenheit (double celsius) |
Converts from degrees Celsius to degrees Fahrenheit. More... | |
static double | CelsiusToKelvin (double celsius) |
Converts from degrees Celsius to degrees Kelvin. More... | |
static double | CelsiusToRankine (double celsius) |
Converts from degrees Celsius to degrees Rankine. More... | |
static double | Constrain (double min, double value, double max) |
Constrain a value between a minimum and a maximum value. | |
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 double | FahrenheitToCelsius (double fahrenheit) |
Converts from degrees Fahrenheit to degrees Celsius. More... | |
static double | FeetToMeters (double measure) |
Converts from feet to meters. More... | |
static double | GaussianRandomNumber (void) |
static double | KelvinToCelsius (double kelvin) |
Converts from degrees Kelvin to degrees Celsius. More... | |
static double | KelvinToFahrenheit (double kelvin) |
Converts from degrees Kelvin to degrees Fahrenheit. More... | |
static double | KelvinToRankine (double kelvin) |
Converts from degrees Kelvin to degrees Rankine. More... | |
static double | MachFromVcalibrated (double vcas, double p, double psl, double rhosl) |
Calculate the Mach number from the calibrated airspeed. More... | |
static double | PitotTotalPressure (double mach, double p) |
Compute the total pressure in front of the Pitot tube. More... | |
static double | RankineToCelsius (double rankine) |
Converts from degrees Rankine to degrees Celsius. More... | |
static double | RankineToKelvin (double rankine) |
Converts from degrees Rankine to degrees Kelvin. More... | |
static double | sign (double num) |
static double | VcalibratedFromMach (double mach, double p, double psl, double rhosl) |
Calculate the calibrated airspeed from the Mach number. More... | |
![]() | |
static short | debug_lvl = 1 |
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 | |
![]() | |
enum | eDistributionType { eUniform =0, eGaussian } |
enum | eNoiseType { ePercent =0, eAbsolute } |
![]() | |
void | Bias (void) |
void | bind (void) |
void | Drift (void) |
void | Gain (void) |
void | Lag (void) |
void | Noise (void) |
void | ProcessSensorSignal (void) |
void | Quantize (void) |
![]() | |
void | Clip (void) |
void | Delay (void) |
![]() | |
void | Debug (int) |
![]() | |
void | CalculateTransformMatrix (void) |
![]() | |
static std::string | CreateIndexedPropertyName (const std::string &Property, int index) |
![]() | |
double | bias |
int | bits |
double | ca |
double | cb |
lag filter coefficient "a" | |
enum JSBSim::FGSensor::eDistributionType | DistributionType |
int | divisions |
double | drift |
double | drift_rate |
bool | fail_high |
bool | fail_low |
bool | fail_stuck |
double | gain |
double | granularity |
double | lag |
double | max |
double | min |
int | noise_type |
double | noise_variance |
enum JSBSim::FGSensor::eNoiseType | NoiseType |
double | PreviousInput |
double | PreviousOutput |
lag filter coefficient "b" | |
std::string | quant_property |
int | quantized |
double | span |
![]() | |
bool | clip |
double | clipmax |
FGPropertyNode_ptr | ClipMaxPropertyNode |
float | clipMaxSign |
double | clipmin |
FGPropertyNode_ptr | ClipMinPropertyNode |
float | clipMinSign |
unsigned int | delay |
double | delay_time |
double | dt |
FGFCS * | fcs |
int | index |
std::vector< std::string > | InitNames |
std::vector< FGPropertyValue * > | InitNodes |
std::vector< float > | InitSigns |
double | Input |
std::vector< std::string > | InputNames |
std::vector< FGPropertyValue * > | InputNodes |
std::vector< float > | InputSigns |
bool | IsOutput |
std::string | Name |
double | Output |
std::vector< double > | output_array |
std::vector< FGPropertyNode_ptr > | OutputNodes |
FGPropertyManager * | PropertyManager |
FGPropertyNode_ptr | treenode |
std::string | Type |
![]() | |
int | axis |
FGMatrix33 | mT |
FGColumnVector3 | vOrient |
![]() | |
static const double | degtorad = 0.017453292519943295769236907684886 |
static const double | fpstokts = 1.0/ktstofps |
static const double | fttom = 0.3048 |
static int | gaussian_random_number_phase = 0 |
static const double | hptoftlbssec = 550.0 |
static const double | in3tom3 = 1.638706E-5 |
static const double | inchtoft = 0.08333333 |
static const double | inhgtopa = 3386.38 |
static const std::string | JSBSim_version = "1.0 " __DATE__ " " __TIME__ |
static const double | kgtolb = 2.20462 |
static const double | kgtoslug = 0.06852168 |
static const double | ktstofps = 1.68781 |
static const double | lbtoslug = 1.0/slugtolb |
static Message | localMsg |
static const double | m3toft3 = 1.0/(fttom*fttom*fttom) |
static double | Mair = 28.9645 |
static unsigned int | messageId = 0 |
static std::queue< Message > | Messages |
static const std::string | needed_cfg_version = "2.0" |
static const double | psftoinhg = 0.014138 |
static const double | psftopa = 47.88 |
static const double | radtodeg = 57.295779513082320876798154814105 |
static double | Reng = 1716.56 |
static double | Rstar = 1545.348 |
static const double | SHRatio = 1.40 |
static const double | slugtolb = 32.174049 |
Encapsulates a Accelerometer component for the flight control system.
Syntax:
Example:
The only required element in the accelerometer definition is the input element. In that case, no degradation would be modeled, and the output would simply be the input.
For noise, if the type is PERCENT, then the value supplied is understood to be a percentage variance. That is, if the number given is 0.05, the variance is understood to be +/-0.05 percent maximum variance. So, the actual value for the accelerometer will be anywhere from 0.95 to 1.05 of the actual "perfect" value at any time - even varying all the way from 0.95 to 1.05 in adjacent frames - whatever the delta time.
Definition at line 136 of file FGAccelerometer.h.