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Nt1310 Unit 1 Lab Report

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INTRODUCTION
1.1 Background
The data handling system on a satellite is used to transmit and receive information to and from the satellite. In addition, the satellite is responsible for processing data from the payload and performing other housekeeping duties. Thus, the satellite data handling system must undergo testing to verify it is working before the satellite can fly its mission. If the data handling system fails, the mission could fail.

1.2 Purpose
The purpose of this lab was to learn how a data handling system works and verify that it was functioning properly. METHODOLOGY
The DC power supply was turned on and set to 10 volts and 0.7 amps. The batteries on the EPS module were disconnected. The DC power supply was connected to the charge …show more content…
The DC power supply was reconnected to the DH module. The functionality of the telemetry delay command, the call sign change command, and the clock set command were verified in the EyasSAT text only interface. The verification of the commands indicated that the DH software was functioning properly. In addition, the IHU temperature was measured as 82 degrees Celsius, well above the ambient room temperature. The IHU temperature reading indicated that the software was functioning properly and able to obtain a thermistor reading, but the reading of 82 degrees Celsius seemed too large. The DC power supply was disconnected from the DH module.

The DH module was connected to the EPS module. The 2-pin connector was connected to the BATT_ENABLE pin on the EPS module. An “ip1” command was sent in the EyasSAT GUI and the “P” line of telemetry began to display. The BI and BV values from the telemetry data were recorded in the bower budget table. Equation (7) shows how to calculate power (P) given the board voltage (BV) in volts and the board current (BI) in milliamps. The units of power are milliwatts. The calculated power was recorded in the bower budget

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