ThrustLab
Simulate electric UAV powertrains and search a public motor, propeller and battery database.
¿Debería usar esto?
Calidad y seguridad
Basado en el análisis automatizado de las definiciones de herramientas y el cumplimiento del protocolo.
Costo de contexto
Este es el número aproximado de tokens que se consumen cada vez que las herramientas del servidor se cargan en el contexto de un modelo. Los recuentos más altos reducen la atención disponible para otras tareas.
Instalar
Instalación con un clic
Agrega esto a tu archivo `claude_desktop_config.json`:
{
"mcpServers": {
"thrustlab": {
"url": "https://thrustlab.com/mcp"
}
}
}Puntos de conexión remotos
https://thrustlab.com/mcpstreamable-httpQué puede hacer
Inventario de herramientas
Herramientas (7)
🟢search_components(component_type, query, limit, offset, sort_by, ...)
Find motors, propellers or batteries in the ThrustLab database. `component_type` is "motor", "propeller" or "battery". `query` is a case-insensitive substring of the part name or its maker ("APC", "T-Motor", "13x6.5"). The maker sits under `spec.brand` for motors and batteries and under `spec.type` for propellers. `limit` is capped at 200 rows a page; when `has_more` is true, pass the returned `next_offset` as `offset` to read the next page. Each row carries its datasheet values, its source and the CC BY 4.0 attribution line. Pass a returned `id` to `simulate_powertrain`.
Esquema de entrada
{
"type": "object",
"properties": {
"component_type": {
"title": "Component Type",
"type": "string"
},
"query": {
"anyOf": [
{
"type": "string"
},
{
"type": "null"
}
],
"default": null,
"title": "Query"
},
"limit": {
"default": 25,
"title": "Limit",
"type": "integer"
},
"offset": {
"default": 0,
"title": "Offset",
"type": "integer"
},
"sort_by": {
"default": "name",
"title": "Sort By",
"type": "string"
},
"sort_order": {
"default": "asc",
"title": "Sort Order",
"type": "string"
}
},
"required": [
"component_type"
],
"title": "search_componentsArguments"
}Esquema de salida
{
"type": "object",
"additionalProperties": true,
"title": "search_componentsDictOutput"
}🟢get_component(component_id)
Read one database row by its id (`comp_…`), with provenance. Propeller rows give diameter, pitch, blade count, weight and maximum rpm. Blade station geometry is never returned.
Esquema de entrada
{
"type": "object",
"properties": {
"component_id": {
"title": "Component Id",
"type": "string"
}
},
"required": [
"component_id"
],
"title": "get_componentArguments"
}Esquema de salida
{
"type": "object",
"additionalProperties": true,
"title": "get_componentDictOutput"
}🟢estimate_propeller(diameter_in, pitch_in, rpm, blades, airspeed_m_s, ...)
Thrust, torque and shaft power for one propeller, from its printed size. A closed-form momentum plus blade-element equation — no motor, no battery, no account. Give the size as it is printed: a 10x5 is `diameter_in=10`, `pitch_in=5`. `chord_ratio` is the chord at 75 % radius over the diameter: 0.065 thin electric, 0.07 sport, 0.10 slow flyer, 0.11 multirotor.
Esquema de entrada
{
"type": "object",
"properties": {
"diameter_in": {
"title": "Diameter In",
"type": "number"
},
"pitch_in": {
"title": "Pitch In",
"type": "number"
},
"rpm": {
"title": "Rpm",
"type": "number"
},
"blades": {
"default": 2,
"title": "Blades",
"type": "integer"
},
"airspeed_m_s": {
"default": 0,
"title": "Airspeed M S",
"type": "number"
},
"altitude_m": {
"default": 0,
"title": "Altitude M",
"type": "number"
},
"chord_ratio": {
"default": 0.065,
"title": "Chord Ratio",
"type": "number"
},
"camber_pct": {
"default": 3.2,
"title": "Camber Pct",
"type": "number"
}
},
"required": [
"diameter_in",
"pitch_in",
"rpm"
],
"title": "estimate_propellerArguments"
}Esquema de salida
{
"type": "object",
"additionalProperties": true,
"title": "estimate_propellerDictOutput"
}🟢simulate_powertrain(powertrain)
Solve one operating point of a whole powertrain on the Fast model. Battery, ESC, motor and propeller are solved together, so the answer is a real thrust and current, not a propeller curve. The numbers come back in `result` (`result.All` = system totals in SI units: thrust N, current A, power W, time s; one entry per rotor; `result.Battery`), with a share URL. No second call is needed to read them.
Esquema de entrada
{
"type": "object",
"properties": {
"powertrain": {
"$ref": "#/$defs/PowertrainInput"
}
},
"required": [
"powertrain"
],
"$defs": {
"PowertrainInput": {
"description": "One powertrain, as the anonymous endpoint accepts it (spec D4).\n\nCatalog components are referenced by their public id (``comp_…``, from\n``search_components``). The propeller may instead be given as a label, which\nis all the Fast model needs.",
"properties": {
"motor_id": {
"description": "Catalog motor public id, e.g. comp_2xK….",
"title": "Motor Id",
"type": "string"
},
"battery_id": {
"description": "Catalog battery public id.",
"title": "Battery Id",
"type": "string"
},
"propeller_id": {
"anyOf": [
{
"type": "string"
},
{
"type": "null"
}
],
"default": null,
"description": "Catalog propeller public id.",
"title": "Propeller Id"
},
"propeller_label": {
"anyOf": [
{
"$ref": "#/$defs/PropellerLabel"
},
{
"type": "null"
}
],
"default": null,
"description": "Use instead of propeller_id to run from the printed size."
},
"rotor_count": {
"default": 1,
"description": "Rotors on the craft.",
"maximum": 16,
"minimum": 1,
"title": "Rotor Count",
"type": "integer"
},
"throttle_pct": {
"default": 100,
"exclusiveMinimum": 0,
"maximum": 100,
"title": "Throttle Pct",
"type": "number"
},
"airspeed_m_s": {
"default": 0,
"description": "0 is a static run.",
"maximum": 300,
"minimum": 0,
"title": "Airspeed M S",
"type": "number"
},
"altitude_m": {
"default": 0,
"maximum": 11000,
"minimum": 0,
"title": "Altitude M",
"type": "number"
}
},
"required": [
"motor_id",
"battery_id"
],
"title": "PowertrainInput",
"type": "object"
},
"PropellerLabel": {
"description": "What is printed on the propeller — all the Fast model reads.\n\nInches and a spoken family name, because that is how a propeller is sold and\nhow a user will say it. :func:`to_schema_label` turns this into the metres\nand the enum ``app.schemas.simulation.PropellerLabel`` declares.",
"properties": {
"diameter_in": {
"description": "Diameter in inches, e.g. 10 for a 10x5.",
"exclusiveMinimum": 0,
"maximum": 400,
"title": "Diameter In",
"type": "number"
},
"pitch_in": {
"description": "Pitch in inches, e.g. 5 for a 10x5.",
"exclusiveMinimum": 0,
"maximum": 400,
"title": "Pitch In",
"type": "number"
},
"num_blades": {
"default": 2,
"description": "Blade count.",
"maximum": 8,
"minimum": 2,
"title": "Num Blades",
"type": "integer"
},
"family": {
"anyOf": [
{
"type": "string"
},
{
"type": "null"
}
],
"default": null,
"description": "Chord-ratio preset: 'thin electric' (0.065 D), 'sport' (0.07 D), 'slow flyer' (0.10 D) or 'multirotor' (0.11 D). Defaults to sport.",
"title": "Family"
},
"chord_ratio": {
"anyOf": [
{
"exclusiveMinimum": 0,
"maximum": 0.5,
"type": "number"
},
{
"type": "null"
}
],
"default": null,
"description": "Chord at 75 % radius over diameter. Give it instead of 'family' (or with family='custom'); the two cannot both be set.",
"title": "Chord Ratio"
},
"camber_pct": {
"anyOf": [
{
"maximum": 8,
"minimum": 0,
"type": "number"
},
{
"type": "null"
}
],
"default": null,
"description": "Section camber in percent. Defaults to 3.2.",
"title": "Camber Pct"
}
},
"required": [
"diameter_in",
"pitch_in"
],
"title": "PropellerLabel",
"type": "object"
}
},
"title": "simulate_powertrainArguments"
}Esquema de salida
{
"type": "object",
"additionalProperties": true,
"title": "simulate_powertrainDictOutput"
}🟢sweep_powertrain(powertrain, sweep)
Solve a powertrain across a throttle or airspeed range, up to 25 points. `sweep.steps` is the NUMBER OF POINTS, not a step size: start 40, stop 100, steps 4 gives 40, 60, 80 and 100. One sweep beats a loop of single points. The points come back in `result.points` with the share URL; no second call is needed to read them.
Esquema de entrada
{
"type": "object",
"properties": {
"powertrain": {
"$ref": "#/$defs/PowertrainInput"
},
"sweep": {
"$ref": "#/$defs/SweepAxis"
}
},
"required": [
"powertrain",
"sweep"
],
"$defs": {
"PowertrainInput": {
"description": "One powertrain, as the anonymous endpoint accepts it (spec D4).\n\nCatalog components are referenced by their public id (``comp_…``, from\n``search_components``). The propeller may instead be given as a label, which\nis all the Fast model needs.",
"properties": {
"motor_id": {
"description": "Catalog motor public id, e.g. comp_2xK….",
"title": "Motor Id",
"type": "string"
},
"battery_id": {
"description": "Catalog battery public id.",
"title": "Battery Id",
"type": "string"
},
"propeller_id": {
"anyOf": [
{
"type": "string"
},
{
"type": "null"
}
],
"default": null,
"description": "Catalog propeller public id.",
"title": "Propeller Id"
},
"propeller_label": {
"anyOf": [
{
"$ref": "#/$defs/PropellerLabel"
},
{
"type": "null"
}
],
"default": null,
"description": "Use instead of propeller_id to run from the printed size."
},
"rotor_count": {
"default": 1,
"description": "Rotors on the craft.",
"maximum": 16,
"minimum": 1,
"title": "Rotor Count",
"type": "integer"
},
"throttle_pct": {
"default": 100,
"exclusiveMinimum": 0,
"maximum": 100,
"title": "Throttle Pct",
"type": "number"
},
"airspeed_m_s": {
"default": 0,
"description": "0 is a static run.",
"maximum": 300,
"minimum": 0,
"title": "Airspeed M S",
"type": "number"
},
"altitude_m": {
"default": 0,
"maximum": 11000,
"minimum": 0,
"title": "Altitude M",
"type": "number"
}
},
"required": [
"motor_id",
"battery_id"
],
"title": "PowertrainInput",
"type": "object"
},
"PropellerLabel": {
"description": "What is printed on the propeller — all the Fast model reads.\n\nInches and a spoken family name, because that is how a propeller is sold and\nhow a user will say it. :func:`to_schema_label` turns this into the metres\nand the enum ``app.schemas.simulation.PropellerLabel`` declares.",
"properties": {
"diameter_in": {
"description": "Diameter in inches, e.g. 10 for a 10x5.",
"exclusiveMinimum": 0,
"maximum": 400,
"title": "Diameter In",
"type": "number"
},
"pitch_in": {
"description": "Pitch in inches, e.g. 5 for a 10x5.",
"exclusiveMinimum": 0,
"maximum": 400,
"title": "Pitch In",
"type": "number"
},
"num_blades": {
"default": 2,
"description": "Blade count.",
"maximum": 8,
"minimum": 2,
"title": "Num Blades",
"type": "integer"
},
"family": {
"anyOf": [
{
"type": "string"
},
{
"type": "null"
}
],
"default": null,
"description": "Chord-ratio preset: 'thin electric' (0.065 D), 'sport' (0.07 D), 'slow flyer' (0.10 D) or 'multirotor' (0.11 D). Defaults to sport.",
"title": "Family"
},
"chord_ratio": {
"anyOf": [
{
"exclusiveMinimum": 0,
"maximum": 0.5,
"type": "number"
},
{
"type": "null"
}
],
"default": null,
"description": "Chord at 75 % radius over diameter. Give it instead of 'family' (or with family='custom'); the two cannot both be set.",
"title": "Chord Ratio"
},
"camber_pct": {
"anyOf": [
{
"maximum": 8,
"minimum": 0,
"type": "number"
},
{
"type": "null"
}
],
"default": null,
"description": "Section camber in percent. Defaults to 3.2.",
"title": "Camber Pct"
}
},
"required": [
"diameter_in",
"pitch_in"
],
"title": "PropellerLabel",
"type": "object"
},
"SweepAxis": {
"description": "A 1-D sweep axis. ``steps`` is the NUMBER OF POINTS, not a step size.",
"properties": {
"parameter": {
"description": "'throttle_pct' or 'airspeed_m_s'.",
"title": "Parameter",
"type": "string"
},
"start": {
"title": "Start",
"type": "number"
},
"stop": {
"title": "Stop",
"type": "number"
},
"steps": {
"description": "Point count, at most 25 anonymous.",
"maximum": 25,
"minimum": 2,
"title": "Steps",
"type": "integer"
}
},
"required": [
"parameter",
"start",
"stop",
"steps"
],
"title": "SweepAxis",
"type": "object"
}
},
"title": "sweep_powertrainArguments"
}Esquema de salida
{
"type": "object",
"additionalProperties": true,
"title": "sweep_powertrainDictOutput"
}🟢get_result(token, simulation_id)
Read a stored result: a share `token` from a run, or a `simulation_id`. `simulation_id` needs a ThrustLab API key in `Authorization: Bearer` and reads only that account's own runs.
Esquema de entrada
{
"type": "object",
"properties": {
"token": {
"anyOf": [
{
"type": "string"
},
{
"type": "null"
}
],
"default": null,
"title": "Token"
},
"simulation_id": {
"anyOf": [
{
"type": "string"
},
{
"type": "null"
}
],
"default": null,
"title": "Simulation Id"
}
},
"title": "get_resultArguments"
}Esquema de salida
{
"type": "object",
"additionalProperties": true,
"title": "get_resultDictOutput"
}🟢get_validation_summary(model)
How accurate a model is, measured against wind-tunnel and bench data. `model` is "fast", "full", or an exact report slug such as "prom-5.3". The numbers are error against measured data by partition and channel, with the envelope they were measured inside. Quote the model name with the number.
Esquema de entrada
{
"type": "object",
"properties": {
"model": {
"default": "full",
"title": "Model",
"type": "string"
}
},
"title": "get_validation_summaryArguments"
}Esquema de salida
{
"type": "object",
"additionalProperties": true,
"title": "get_validation_summaryDictOutput"
}Comunidad
Evidencia