FlightGear next
|
Encapsulates a filter for the flight control system. More...
#include <FGFilter.h>
Inherits JSBSim::FGFCSComponent.
Public Member Functions | |
FGFilter (FGFCS *fcs, Element *element) | |
~FGFilter () | |
bool | Run (void) override |
void | ResetPastStates (void) override |
![]() | |
FGFCSComponent (FGFCS *fcs, Element *el) | |
Constructor. | |
virtual | ~FGFCSComponent () |
Destructor. | |
virtual void | SetOutput (void) |
double | GetOutput (void) const |
std::string | GetName (void) const |
std::string | GetType (void) const |
virtual double | GetOutputPct (void) const |
![]() | |
FGJSBBase () | |
Constructor for FGJSBBase. | |
virtual | ~FGJSBBase () |
Destructor for FGJSBBase. | |
void | PutMessage (const Message &msg) |
Places a Message structure on the Message queue. | |
void | PutMessage (const std::string &text) |
Creates a message with the given text and places it on the queue. | |
void | PutMessage (const std::string &text, bool bVal) |
Creates a message with the given text and boolean value and places it on the queue. | |
void | PutMessage (const std::string &text, int iVal) |
Creates a message with the given text and integer value and places it on the queue. | |
void | PutMessage (const std::string &text, double dVal) |
Creates a message with the given text and double value and places it on the queue. | |
int | SomeMessages (void) const |
Reads the message on the queue (but does not delete it). | |
void | ProcessMessage (void) |
Reads the message on the queue and removes it from the queue. | |
Message * | ProcessNextMessage (void) |
Reads the next message on the queue and removes it from the queue. | |
void | disableHighLighting (void) |
Disables highlighting in the console output. | |
Additional Inherited Members | |
![]() | |
enum | { eL = 1 , eM , eN } |
Moments L, M, N. More... | |
enum | { eP = 1 , eQ , eR } |
Rates P, Q, R. More... | |
enum | { eU = 1 , eV , eW } |
Velocities U, V, W. More... | |
enum | { eX = 1 , eY , eZ } |
Positions X, Y, Z. More... | |
enum | { ePhi = 1 , eTht , ePsi } |
Euler angles Phi, Theta, Psi. More... | |
enum | { eDrag = 1 , eSide , eLift } |
Stability axis forces, Drag, Side force, Lift. More... | |
enum | { eRoll = 1 , ePitch , eYaw } |
Local frame orientation Roll, Pitch, Yaw. More... | |
enum | { eNorth = 1 , eEast , eDown } |
Local frame position North, East, Down. More... | |
enum | { eLat = 1 , eLong , eRad } |
Locations Radius, Latitude, Longitude. More... | |
enum | { inNone = 0 , inDegrees , inRadians , inMeters , inFeet } |
Conversion specifiers. More... | |
static const std::string & | GetVersion (void) |
Returns the version number of JSBSim. | |
static constexpr double | KelvinToFahrenheit (double kelvin) |
Converts from degrees Kelvin to degrees Fahrenheit. | |
static constexpr double | CelsiusToRankine (double celsius) |
Converts from degrees Celsius to degrees Rankine. | |
static constexpr double | RankineToCelsius (double rankine) |
Converts from degrees Rankine to degrees Celsius. | |
static constexpr double | KelvinToRankine (double kelvin) |
Converts from degrees Kelvin to degrees Rankine. | |
static constexpr double | RankineToKelvin (double rankine) |
Converts from degrees Rankine to degrees Kelvin. | |
static constexpr double | FahrenheitToCelsius (double fahrenheit) |
Converts from degrees Fahrenheit to degrees Celsius. | |
static constexpr double | CelsiusToFahrenheit (double celsius) |
Converts from degrees Celsius to degrees Fahrenheit. | |
static constexpr double | CelsiusToKelvin (double celsius) |
Converts from degrees Celsius to degrees Kelvin. | |
static constexpr double | KelvinToCelsius (double kelvin) |
Converts from degrees Kelvin to degrees Celsius. | |
static constexpr double | FeetToMeters (double measure) |
Converts from feet to meters. | |
static double | PitotTotalPressure (double mach, double p) |
Compute the total pressure in front of the Pitot tube. | |
static double | MachFromImpactPressure (double qc, double p) |
Compute the Mach number from the differential pressure (qc) and the static pressure. | |
static double | VcalibratedFromMach (double mach, double p) |
Calculate the calibrated airspeed from the Mach number. | |
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). | |
static bool | EqualToRoundoff (double a, double b) |
Finite precision comparison. | |
static bool | EqualToRoundoff (float a, float b) |
Finite precision comparison. | |
static bool | EqualToRoundoff (float a, double b) |
Finite precision comparison. | |
static bool | EqualToRoundoff (double a, float b) |
Finite precision comparison. | |
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 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 |
![]() | |
void | Delay (void) |
void | Clip (void) |
void | CheckInputNodes (size_t MinNodes, size_t MaxNodes, Element *el) |
virtual void | bind (Element *el) |
static std::string | CreateIndexedPropertyName (const std::string &Property, int index) |
![]() | |
FGFCS * | fcs |
FGPropertyManager * | PropertyManager |
std::vector< FGPropertyNode_ptr > | OutputNodes |
FGParameter_ptr | ClipMin |
FGParameter_ptr | ClipMax |
std::vector< FGPropertyValue_ptr > | InitNodes |
std::vector< FGPropertyValue_ptr > | InputNodes |
std::vector< double > | output_array |
std::string | Type |
std::string | Name |
double | Input |
double | Output |
double | delay_time |
unsigned int | delay |
int | index |
double | dt |
bool | clip |
bool | cyclic_clip |
static Message | localMsg |
static std::queue< Message > | Messages |
static unsigned int | messageId = 0 |
static constexpr double | radtodeg = 180. / 3.14159265358979323846 |
static constexpr double | degtorad = 3.14159265358979323846 / 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. | |
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 |
Encapsulates a filter for the flight control system.
The filter component can simulate any first or second order filter. The Tustin substitution is used to take filter definitions from LaPlace space to the time domain. The general format for a filter specification is:
The numerical integration of filters is made by a Runge-Kutta scheme of order 2 except for the second order filter which uses an RK scheme of order 3.
For a lag filter of the form
As an example, for the specific filter
For a lead-lag filter of the form
For a washout filter of the form
For a second order filter of the form
For an integrator of the form
For the integrator, the trigger features the following behavior. If the trigger property value is:
By default, the integration scheme is the trapezoidal scheme.
An integrator is equivalent to a PID with the following parameters:
As a consequence, JSBSim internally uses PID controllers to simulate INTEGRATOR filters.
In all the filter specifications above, an <output> element is also seen. This is so that the last component in a "string" can copy its value to the appropriate output, such as the elevator, or speedbrake, etc.
Definition at line 215 of file FGFilter.h.
Definition at line 51 of file FGFilter.cpp.
JSBSim::FGFilter::~FGFilter | ( | ) |
Definition at line 76 of file FGFilter.cpp.
|
overridevirtual |
Reimplemented from JSBSim::FGFCSComponent.
Definition at line 83 of file FGFilter.cpp.
|
overridevirtual |
Reimplemented from JSBSim::FGFCSComponent.
Definition at line 147 of file FGFilter.cpp.