The invention discloses a method for enhancing the in-
orbit reliability of a moonlet, relates to the field of the in-
orbit reliability guaranteeing of a
spacecraft, and solves the problems of poor reliability, low working efficiency and the like since the moonlet is likely to be subjected to a situation that one-
machine component is out of control or a whole
spacecraft is out of control when the moonlet carries out in-
orbit task execution. Interruption is used for solving the problem of the abnormal communication of the moonlet,
software on
satellite is used for automatically solving the problem that an RS422
bus, a
CAN bus and a PPS (Pulse Per Second)
signal are continuously abnormal. When certain one
machine is subjected to abnormal communication, after interruption frequencies achieve apreset threshold value, the
communication interface of the one
machine is shielded through a continuous interruption way, and the one-machine component is restarted. Since an abnormity
processing method is carried out in
application software, an effect of quick response and abnormal
processing can be achieved. The problem that the abnormity is only solved through the injection of a remote controlinstruction on the ground after the
satellite rises to the
sky, and the reliability and the stability of the in-orbit operation of the moonlet are effectively improved.