vehicle_profile
Infers aircraft frame type, motor count, battery cells/capacity, hover throttle, and thrust-to-weight from ArduPilot logs to evaluate power margin and physical performance.
Instructions
Physical / architecture profile of the aircraft inferred from the log.
Frame class & type, motor count, battery cells/capacity, and — the key physical insight — the hover throttle and resulting power margin / thrust-to-weight. Use this to reason about the craft physically and to combine with real-world details the user gives (weight, prop diameter, motor KV, wind).
Input Schema
| Name | Required | Description | Default |
|---|---|---|---|
| path | Yes |
Output Schema
| Name | Required | Description | Default |
|---|---|---|---|
| path | Yes | ||
| notes | No | ||
| assessment | No | Plain-language physical observations (e.g. 'underpowered'). | |
| frame_type | No | ||
| references | No | ||
| frame_class | No | ||
| motor_count | No | Number of lift motors implied by the frame. | |
| vehicle_kind | No | ||
| vehicle_type | No | ||
| battery_cells | No | Estimated LiPo cell count (S). | |
| max_voltage_v | No | ||
| hover_throttle | No | Throttle (0..1) needed to hover; from MOT_THST_HOVER or measured. | |
| frame_type_name | No | ||
| firmware_version | No | ||
| frame_class_name | No | ||
| power_margin_pct | No | Spare throttle above hover (100*(1-hover)); low = underpowered. | |
| nominal_voltage_v | No | ||
| battery_capacity_mah | No | ||
| thrust_to_weight_estimate | No | Rough max-thrust/weight (~1/hover_throttle). |