Spacecraft Actuator Diagnosis with Principal Component Analysis: Application to the Rendez-Vous Phase of the Mars Sample Return Mission

Algorithm 2

The fault detection algorithm.

        Inputs: , , .

        Outputs: SPE, ,

()      Calculate the detection threshold  

()      

()      for ( to ) do

()        Calculate  :

()        

()        if    then

()          .

()        else

()          .

()     end

()    end