| Satellite Subsystems » Electrical » Telemetry | ||
The purpose of the telemetry network aboard BLUEsat is to capture the readings of up to 64 sensors at various points around the satellite. The readings of all the sensors are assembled into a telemetry package, which is streamed down to earth continuously through the beacon. The telemetry package allows the satellite operators to diagnose or pre-empt potential problems and develop remedies, and simply to monitor that the satellite is functioning correctly throughout.
The sensors aboard BLUEsat take measurements of things like battery and solar panel voltage and current, temperatures at each face of the satellite and at internal points, and the statuses of various subsystems of the satellite, for example, receiver signal strength.
The network comprises a two-wire electrical bus using the PHILIPS I2C protocol, to which individual telemetry nodes are attached. Each node will have a bus interface connected, with appropriate logic, to a sensor. The reading of each sensor can be read by performing a read operation to the sensor's unique I2C bus address from the Flight Computer (FC). The FC is responsible for regularly collecting sensor readings, assembling a telemetry frame, and transmitting this down to earth on the beacon.
BLUEsat Telemetry Architecture
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| Author: Chris Walsh © The Author, the BLUEsat project or UNSW. All rights reserved. Last Modified: September 18 2006 02:03:00. |