33 #ifndef FGMAGNETOMETER_H 34 #define FGMAGNETOMETER_H 41 #include "models/FGPropagate.h" 42 #include "models/FGMassBalance.h" 43 #include "models/FGInertial.h" 44 #include "math/FGColumnVector3.h" 45 #include "math/FGMatrix33.h" 46 #include "FGSensorOrientation.h" 52 #define ID_MAGNETOMETER "$Id: FGMagnetometer.h,v 1.5 2013/11/24 11:40:57 bcoconni Exp $" 142 void updateInertialMag(
void);
147 unsigned long int date;
149 int INERTIAL_UPDATE_RATE;
151 void Debug(
int from);
Encapsulates a magnetometer component for the flight control system.
Models inertial forces (e.g.
Encapsulates a Sensor component for the flight control system.
Models the EOM and integration/propagation of state.
This class implements a 3 element column vector.
Encapsulates the Flight Control System (FCS) functionality.
Encapsulates a SensorOrientation capability for a sensor.
Models weight, balance and moment of inertia information.