A Spacecraft On-orbit Abnormal Alarm and Fault Diagnosis System
A fault diagnosis system and abnormal alarm technology, applied in the field of aerospace fault diagnosis, can solve problems such as uncertainty, difficult description, and difficulty in penumbra description.
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[0057] Example 1: Bus voltage drop (undervoltage) in the lighting area
[0058] The normal value of the bus voltage in the light area should be 42V±0.5V. The reasons for the voltage drop are:
[0059] (1) The fault of the shunt regulator causes the shunt value to be too large, the output power of the solar cell array is shunted, the bus voltage control fails, and the load cannot be powered. Check the error signal output of the busbar: north VN4 (south VN12) ≥ 6V. Whether the -12V power supply is open circuit (telemetry code).
[0060] (2) INTO MOON SHADOW. (Normal phenomenon, calculated according to calculation and forecast)
[0061] (3) The load current on the bus is overcurrent. It cannot return to normal until the short circuit factor is eliminated
[0062] (4) The solar panel reverses and stops. Return the sailboard to its normal state.
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