Disclosed is an automatic failure handling and protection method of a deep
space probe global navigation chart (GNC)
system base on a
layered structure. The automatic failure handling and protection method of the deep
space probe GNC
system base on the
layered structure comprises the steps of carrying out hardware protection to avoid a failure which can result in permanent damage or invalidation of other parts or other parts inside a part according to a result of
failure mode and effects analysis (FMEA), judging whether the data of measuring points are normal with an
infrared ray method for other failures, marking the states of parts and handling the data and state information to a controller for analyzing of
system-level failures; carrying out failure analyzing according to the state information and the data of the measuring points handed to the controller: if
hardware redundancy or analysis redundancy exists, a failure part is switched to a normal redundancy part; if the
hardware redundancy or the analysis redundancy
dose not exist, the next step is carried out; switching to a counter-glow orientation mode when the prior step can not position a failure source or no redundant
backup can replace the failure source and gesture is pretty poor and directing is out of control, switching off equipments not necessary for flying of a deep
space probe to reduce
power consumption, and switching off a self-locking valve and switching to a control-stop mode to reduce
propellant consumption of the probe when the probe is out of control, a pushing system spray gas at random and star bodies roll.