modelForceMoment
partial force model that computes aerodynamic relavent properties, still required to define F_b, M_B
Extends from Parts.ForceMoment (A rigid body force and moment.).
Parameters
| Type | Name | Default | Description |
|---|
| SI.Velocity | vtTol | 0.01 | when to ignore aerodynamics |
| SI.Area | s | | reference area |
| SI.Length | cBar | | average chord |
| SI.Length | b | | span |
| Real | epsilon | 1e-10 | |
Components
| Type | Name | Default | Description |
|---|
| SI.Force[3] | F_b (from ForceMoment) | | |
| SI.Torque[3] | M_b (from ForceMoment) | | |
| World.WorldBase | world | | |
| SI.Velocity[3] | vR_b | | relative air velocity resolved in body frame |
| SI.Acceleration[3] | aR_b | | relative air acceleration resolved in body frame |
| SI.Velocity | vt | | true air velocity |
| SI.Acceleration | vtDot | | true air velocity derivative |
| SI.Pressure | qBar | | dynamics pressure |
| SI.Angle | alpha | | angle of attack |
| SI.AngularVelocity | alphaDot | | derivative of angle of attack |
| SI.Angle | beta | | side slip angle |
| SI.AngularVelocity | betaDot | | derivative of side slip angle |
| SI.AngularVelocity | p | | body roll rate |
| SI.AngularVelocity | q | | body pitch rate |
| SI.AngularVelocity | r | | body yaw rate |
| SI.Angle | alpha_deg | | angle of attack, deg |
| SI.Angle | beta_deg | | side slip, deg |
| Real[3,3] | C_bs | | stability to body frame |
| Real[3,3] | C_bw | | wind to body frame |
| Real[3] | wind | | wind |