WOLFRAM SYSTEM MODELER
FlightDataOutFlight data output |
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Wolfram Language
In[1]:=
SystemModel["Aircraft.Physical.FixedWing.Interfaces.FlightDataOut"]
Out[1]:=
Information
This connector is an output port for the variables stored in the FlightData record.
Connectors (28)
 |
mTot |
Type: RealOutput Description: Aircraft total mass |
|---|---|---|
|
Ixx |
Type: RealOutput Description: Aircraft roll moment of inertia |
|
Iyy |
Type: RealOutput Description: Aircraft pitch moment of inertia |
|
Izz |
Type: RealOutput Description: Aircraft yaw moment of inertia |
|
Ixy |
Type: RealOutput Description: Aircraft xy product of inertia |
|
Ixz |
Type: RealOutput Description: Aircraft xz product of inertia |
|
Iyz |
Type: RealOutput Description: Aircraft yz product of inertia |
|
loadFactor |
Type: RealOutput Description: Aircraft load factor (= G-force) |
|
alt |
Type: RealOutput Description: Geometric altitude |
|
positionAC |
Type: RealOutput[3] Description: Aircraft position in world frame |
|
phi |
Type: RealOutput Description: Roll angle |
|
theta |
Type: RealOutput Description: Pitch angle |
|
psi |
Type: RealOutput Description: Yaw angle (heading) |
|
alpha |
Type: RealOutput Description: Angle of attack |
|
beta |
Type: RealOutput Description: Sideslip angle |
|
track |
Type: RealOutput Description: Track angle |
|
gamma |
Type: RealOutput Description: Flight path angle |
|
vWorld |
Type: RealOutput[3] Description: Velocity components (v_x, v_y and v_z) in world frame |
|
vBody |
Type: RealOutput[3] Description: Velocity components (u, v and w) in body frame |
|
vTot |
Type: RealOutput Description: Total velocity |
|
vGround |
Type: RealOutput Description: Ground speed |
|
mach |
Type: RealOutput Description: Mach number |
|
pAlt |
Type: RealOutput Description: Static pressure at altitude |
|
Talt |
Type: RealOutput Description: Static temperature at altitude |
|
rhoAlt |
Type: RealOutput Description: Air density at altitude |
|
aAlt |
Type: RealOutput Description: Speed of sound at altitude |
|
muAlt |
Type: RealOutput Description: Air viscosity at altitude |
|
qAC |
Type: RealOutput Description: Global dynamic pressure at altitude at flight speed |
Connector Variables (29)
| flightData |
Causality: Input Type: FlightData Description: Global flight data variables (measured at the aircraft center of mass location) |
|---|---|
| mTot |
Causality: None Type: RealOutput (kg) Description: Aircraft total mass |
| Ixx |
Causality: None Type: RealOutput (kg⋅m²) Description: Aircraft roll moment of inertia |
| Iyy |
Causality: None Type: RealOutput (kg⋅m²) Description: Aircraft pitch moment of inertia |
| Izz |
Causality: None Type: RealOutput (kg⋅m²) Description: Aircraft yaw moment of inertia |
| Ixy |
Causality: None Type: RealOutput (kg⋅m²) Description: Aircraft xy product of inertia |
| Ixz |
Causality: None Type: RealOutput (kg⋅m²) Description: Aircraft xz product of inertia |
| Iyz |
Causality: None Type: RealOutput (kg⋅m²) Description: Aircraft yz product of inertia |
| loadFactor |
Causality: None Type: RealOutput Description: Aircraft load factor (= G-force) |
| alt |
Causality: None Type: RealOutput (m) Description: Geometric altitude |
| positionAC |
Causality: None Type: RealOutput[3] (m) Description: Aircraft position in world frame |
| phi |
Causality: None Type: RealOutput (rad) Description: Roll angle |
| theta |
Causality: None Type: RealOutput (rad) Description: Pitch angle |
| psi |
Causality: None Type: RealOutput (rad) Description: Yaw angle (heading) |
| alpha |
Causality: None Type: RealOutput (rad) Description: Angle of attack |
| beta |
Causality: None Type: RealOutput (rad) Description: Sideslip angle |
| track |
Causality: None Type: RealOutput (rad) Description: Track angle |
| gamma |
Causality: None Type: RealOutput (rad) Description: Flight path angle |
| vWorld |
Causality: None Type: RealOutput[3] (m/s) Description: Velocity components (v_x, v_y and v_z) in world frame |
| vBody |
Causality: None Type: RealOutput[3] (m/s) Description: Velocity components (u, v and w) in body frame |
| vTot |
Causality: None Type: RealOutput (m/s) Description: Total velocity |
| vGround |
Causality: None Type: RealOutput (m/s) Description: Ground speed |
| mach |
Causality: None Type: RealOutput Description: Mach number |
| pAlt |
Causality: None Type: RealOutput (Pa) Description: Static pressure at altitude |
| Talt |
Causality: None Type: RealOutput (K) Description: Static temperature at altitude |
| rhoAlt |
Causality: None Type: RealOutput (kg/m³) Description: Air density at altitude |
| aAlt |
Causality: None Type: RealOutput (m/s) Description: Speed of sound at altitude |
| muAlt |
Causality: None Type: RealOutput (Pa⋅s) Description: Air viscosity at altitude |
| qAC |
Causality: None Type: RealOutput (Pa) Description: Global dynamic pressure at altitude at flight speed |
Used in Components (1)
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Aircraft.Physical.FixedWing.Interfaces Interface for a complete aircraft model |