landing_performance
Calculate landing distance for aircraft using weight, altitude, temperature, wind, runway slope, and condition. Obtain V-speeds, air distance, ground roll, and factored distances.
Instructions
Calculate landing distance for given conditions.
Args: weight_kg: Landing weight in kg pressure_altitude_ft: Airport pressure altitude in feet temperature_c: Outside air temperature in Celsius wind_kts: Headwind (+) or tailwind (-) in knots runway_slope_pct: Runway slope in percent (+ uphill) runway_condition: "dry", "wet", or "contaminated" cl_max_landing: Maximum lift coefficient in landing config wing_area_m2: Wing reference area in m² vref_factor: Approach speed factor (typically 1.3) approach_angle_deg: Approach angle in degrees
Returns: Formatted string with landing performance calculations including V-speeds, air distance from 50 ft, ground roll, and factored distances.
Raises: No exceptions are raised directly; errors are returned as formatted strings.
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| weight_kg | Yes | ||
| pressure_altitude_ft | Yes | ||
| temperature_c | Yes | ||
| wind_kts | No | ||
| runway_slope_pct | No | ||
| runway_condition | No | dry | |
| cl_max_landing | No | ||
| wing_area_m2 | No | ||
| vref_factor | No | ||
| approach_angle_deg | No |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| result | Yes |