JSBSim Flight Dynamics Model 1.0 (23 February 2013)
An Open Source Flight Dynamics and Control Software Library in C++

FGPropagate::VehicleState Struct Reference

The current vehicle state vector structure contains the translational and angular position, and the translational and angular velocity. More...

#include <FGPropagate.h>

Collaboration diagram for FGPropagate::VehicleState:

List of all members.

Public Attributes

deque< FGColumnVector3dqInertialVelocity
deque< FGColumnVector3dqPQRidot
deque< FGQuaterniondqQtrndot
deque< FGColumnVector3dqUVWidot
FGQuaternion qAttitudeECI
 The current orientation of the vehicle, that is, the orientation of the body frame relative to the inertial (ECI) frame.
FGQuaternion qAttitudeLocal
 The current orientation of the vehicle, that is, the orientation of the body frame relative to the local, NED frame.
FGColumnVector3 vInertialPosition
FGColumnVector3 vInertialVelocity
FGLocation vLocation
 Represents the current location of the vehicle in Earth centered Earth fixed (ECEF) frame.
FGColumnVector3 vPQR
 The angular velocity vector for the vehicle relative to the ECEF frame, expressed in the body frame.
FGColumnVector3 vPQRi
 The angular velocity vector for the vehicle body frame relative to the ECI frame, expressed in the body frame.
FGColumnVector3 vUVW
 The velocity vector of the vehicle with respect to the ECEF frame, expressed in the body system.

Detailed Description

Definition at line 108 of file FGPropagate.h.


Member Data Documentation

units rad/sec

Definition at line 122 of file FGPropagate.h.

Referenced by FGPropagate::GetPQR(), and FGPropagate::Run().

units rad/sec

Definition at line 127 of file FGPropagate.h.

Referenced by FGPropagate::GetPQRi(), and FGPropagate::Run().

units ft/sec

Definition at line 117 of file FGPropagate.h.

Referenced by FGPropagate::GetECEFVelocity(), FGPropagate::GetUVW(), and FGPropagate::Run().


The documentation for this struct was generated from the following files: