recordCoefficientsAndDerivativesSimple
Components
| Type | Name | Default | Description |
|---|
| Real | alphaStall_deg | | stall angle of attack |
| Real | CL0 | | |
| Real | CLa | | CL alpha slope |
| Real | CD0 | | minimum drag |
| Real | CDCL | | CL^2 term for drag polar |
| Real | CYb | | side slipe effect on side force |
| Real | Clp | | roll damping, <0 for stability |
| Real | Clda | | aileron effect on roll |
| Real | Cmq | | pitch damping, <0 for stability |
| Real | Cma | | alpha effect on pitch, <0 for stability |
| Real | Cmde | | elevator effect on pitch |
| Real | Cnb | | weather cocking stability >0 for stability |
| Real | Cnr | | yaw damping, <0 for stability |
| Real | Cndr | | rudder effecto on yaw |