weight_and_balance
Compute the center of gravity of an aircraft and confirm it falls within the allowable forward and aft limits for safe flight.
Instructions
Calculate aircraft center of gravity and verify within limits.
Args: basic_empty_weight_kg: Basic empty weight in kg basic_empty_arm_m: Basic empty weight CG arm (from datum) in meters fuel_kg: Fuel load in kg fuel_arm_m: Fuel tank CG arm in meters payload_items: List of payload items, each with keys: - weight_kg: Weight in kg - arm_m: CG arm in meters - name: Item name (optional) forward_cg_limit_m: Forward CG limit (optional) aft_cg_limit_m: Aft CG limit (optional) max_takeoff_weight_kg: Maximum takeoff weight (optional) mac_m: Mean aerodynamic chord length (optional, for %MAC calculation) lemac_m: Leading edge of MAC position (optional, for %MAC calculation)
Returns: Formatted string with weight and balance calculation results.
Raises: No exceptions are raised directly; errors are returned as formatted strings.
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| basic_empty_weight_kg | Yes | ||
| basic_empty_arm_m | Yes | ||
| fuel_kg | Yes | ||
| fuel_arm_m | Yes | ||
| payload_items | Yes | ||
| forward_cg_limit_m | No | ||
| aft_cg_limit_m | No | ||
| max_takeoff_weight_kg | No | ||
| mac_m | No | ||
| lemac_m | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| result | Yes |