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Example: Telemetry from a spacecraft to a ground station
This example demonstrates a complete CCSDS telemetry chain:
Spacecraft Side: 1. Generate telemetry data as Space Packets (SPP) 2. Frame packets into TM Transfer Frames (TMDL) 3. Wrap frames as CADUs (ASM + optional randomization) 4. Transmit over a simulated RF link Ground Station Side: 1. Receive CADUs from the RF link 2. Unwrap to extract TM Transfer Frames 3. Demultiplex virtual channels 4. Extract original Space Packets from frames
The spacecraft uses two virtual channels:
- VC0 (priority 3): Housekeeping telemetry (APID 100)
- VC1 (priority 1): Science payload data (APID 200)
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