Schema | satellite-anomaly-mcp

satellite-anomaly-mcp

Describes the environment variables required to run the server.

Name	Required	Description	Default
No arguments

Guidance the server publishes about itself, which clients place ahead of the tool catalog so the model reads it before choosing anything.

This server publishes no instructions, or was last inspected before Glama recorded them.

Features and capabilities supported by this server

Protocol revision2025-11-25

Functions exposed to the LLM to take actions

Name	Description
evaluate_telemetryB	Evaluates satellite telemetry frame through safety envelope, space-weather filter, and sensor isolation.
simulate_scenarioB	Simulates satellite fault scenarios (space_weather, sensor_fault, true_anomaly, adcs_tumble).
detect_novelty_anomalyC	Runs density-based anomaly detector for telemetry features out of distribution.
isolate_fault_componentC	Issues command to isolate suspect satellite component or switch to redundant subsystem.
trigger_safe_modeB	Triggers emergency spacecraft safe-mode sequence to protect bus hardware.
generate_diagnostic_reportB	Generates structured satellite anomaly diagnosis summary for flight operations controllers.
verify_ground_station_authB	Verifies Ground Station security context for executing sensitive safety maneuvers.

Interactive templates invoked by user choice

Name	Description
`triage_fault`	Guided flight operations prompt for assessing telemetry anomalies and recommending isolation steps.
`generate_pass_summary`	Generates ground station pass summary prompt after satellite contact.

Contextual data attached and managed by the client

Name	Description
`Current Spacecraft Telemetry Vector`	Provides latest real-time sensor vector for SAT-ALPHA-1
`Hard Safety Envelope Thresholds`	Configured hardware limits for bus voltage, battery temp, and tumbling rate
`Constellation Health Matrix`	Status summary across active constellation satellites