 |
JSBSim Flight Dynamics Model
1.0 (02 March 2017)
An Open Source Flight Dynamics and Control Software Library in C++
|
|
JSBSim Flight Dynamics Model
1.0 (02 March 2017)
An Open Source Flight Dynamics and Control Software Library in C++
|
Collaboration diagram for FGAccelerations::Inputs:Public Attributes | |
| double | DeltaT |
| Time step. | |
| FGColumnVector3 | Force |
| Total forces applied to the body except friction and gravity (expressed in the body frame) | |
| double | GAccel |
| Gravity intensity assuming the Earth is spherical. | |
| FGColumnVector3 | GroundForce |
| Forces generated by the ground normal reactions expressed in the body frame. Does not account for friction. | |
| FGColumnVector3 | GroundMoment |
| Moments generated by the ground normal reactions expressed in the body frame. Does not account for friction. | |
| FGMatrix33 | J |
| The body inertia matrix expressed in the body frame. | |
| FGColumnVector3 | J2Grav |
| Gravity intensity vector using WGS84 formulas (expressed in the ECEF frame). | |
| FGMatrix33 | Jinv |
| The inverse of the inertia matrix J. | |
| double | Mass |
| Body mass. | |
| FGColumnVector3 | Moment |
| Total moments applied to the body except friction and gravity (expressed in the body frame) | |
| std::vector< LagrangeMultiplier * > * | MultipliersList |
| List of Lagrange multipliers set by FGLGear for friction forces calculations. | |
| FGMatrix33 | Tb2i |
| Transformation matrix from the Body to the ECI frame. | |
| FGMatrix33 | Tec2b |
| Transformation matrix from the ECEF to the Body frame. | |
| FGMatrix33 | Tec2i |
| Transformation matrix from the ECEF to the ECI frame. | |
| FGColumnVector3 | TerrainAngularVel |
| Terrain angular velocities with respect to the local frame (expressed in the ECEF frame). | |
| FGColumnVector3 | TerrainVelocity |
| Terrain velocities with respect to the local frame (expressed in the ECEF frame). | |
| FGMatrix33 | Ti2b |
| Transformation matrix from the ECI to the Body frame. | |
| FGColumnVector3 | vInertialPosition |
| Body position (X,Y,Z) measured in the ECI frame. | |
| FGColumnVector3 | vOmegaPlanet |
| Earth rotating vector (expressed in the ECI frame). | |
| FGColumnVector3 | vPQR |
| Angular velocities of the body with respect to the local frame (expressed in the body frame). | |
| FGColumnVector3 | vPQRi |
| Angular velocities of the body with respect to the ECI frame (expressed in the body frame). | |
| FGColumnVector3 | vUVW |
| Velocities of the body with respect to the local frame (expressed in the body frame). | |
Definition at line 339 of file FGAccelerations.h.
1.8.13 