ThrustLab
Simulate electric UAV powertrains and search a public motor, propeller and battery database.
Sollte ich dies verwenden
Qualität und Sicherheit
Basierend auf einer automatisierten Analyse der Tool-Definitionen und der Einhaltung des Protokolls.
Kontextkosten
Dies ist die ungefähre Anzahl der Tokens, die jedes Mal verbraucht werden, wenn die Tools des Servers in den Kontext eines Modells geladen werden. Höhere Werte verringern die Aufmerksamkeit, die für andere Aufgaben verfügbar ist.
Installieren
Installation mit einem Klick
Fügen Sie dies Ihrer Datei `claude_desktop_config.json` hinzu:
{
"mcpServers": {
"thrustlab": {
"url": "https://thrustlab.com/mcp"
}
}
}Remote-Endpunkte
https://thrustlab.com/mcpstreamable-httpWas es kann
Tool-Inventar
Tools (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`.
Eingabe-Schema
{
"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"
}Ausgabe-Schema
{
"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.
Eingabe-Schema
{
"type": "object",
"properties": {
"component_id": {
"title": "Component Id",
"type": "string"
}
},
"required": [
"component_id"
],
"title": "get_componentArguments"
}Ausgabe-Schema
{
"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.
Eingabe-Schema
{
"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"
}Ausgabe-Schema
{
"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.
Eingabe-Schema
{
"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"
}Ausgabe-Schema
{
"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.
Eingabe-Schema
{
"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"
}Ausgabe-Schema
{
"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.
Eingabe-Schema
{
"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"
}Ausgabe-Schema
{
"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.
Eingabe-Schema
{
"type": "object",
"properties": {
"model": {
"default": "full",
"title": "Model",
"type": "string"
}
},
"title": "get_validation_summaryArguments"
}Ausgabe-Schema
{
"type": "object",
"additionalProperties": true,
"title": "get_validation_summaryDictOutput"
}Community
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