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

Algorithm 3

The fault isolation algorithm.

        Inputs: , .

        Outputs: , .

()      for ( to ) do

()        for ( to ) do

()         Calculate  :

()         

()         Calculate  :

()         

()         

()         if  ()  then

()           The Rth variable is faulty.

()      end

()     end

()   end