avl.trim
Solve for angle of attack and one control deflection to achieve target lift and pitching moment coefficients at zero sideslip and body rates.
Instructions
Solve alpha and one existing CONTROL for target CL/Cm at zero beta/body rates. CONTROL values retain section gains, not automatically physical deflection degrees. Bounds accept/reject the native solution, not constrain iterations. Success requires residual/bounds checks and a fresh fixed-condition solve. Moments use the explicit geometry/override reference point, not an inferred CG. No mass/thrust balance.
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| outputs | No | ||
| request | Yes | ||
| case_name | No | trim | |
| model_path | Yes | ||
| references | No | ||
| length_unit | No | unspecified | |
| timeout_seconds | No |