{ the [ core Differential Equation governing the behavior of the Satellite ] }
And we shall now re-write this equation in this format :
for our usage below .
we can now express the { first-derivative of [ Theta ] with respect to time } as :
yielding :
Consequently :
Substituting this into the equation immediately above then yields us this relation :
And consequently , we have this final equation :
for the { second-derivative of [ Theta ] with respect to time } .
Taking the derivative thereof with respect to time then yields us this relation :
yielding :
Therefore :
and
Substituting these into the equation immediately before then yields us this relation :
And consequently , we have this final equation :
for the { second-derivative of [ R ] with respect to time } .
Let us recall that we have already established above :
and
Substituting these into the equation immediately before then yields us this relation :
yielding :
This is an important equation that we shall be coming back to in Section XXXIV of this paper ,
Let us now multiply throughout by :
We then arrive at this final equation below :