LFState:

Path: FormationFlying/Coord

% Leader-follower Hills state
 Computes the position and velocity of a satellite in the Hills frame for a
 leader/follower formation given the distance from the center (d), the number
 of spacecraft (nSC), and the order in the line.

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   Form:
   state = LFState( d, nSC, order )
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   Inputs
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   d     	(1,1)     Distance from reference point (km)
   nSC     (1,1)     Number of spacecraft
   order   (1,1)     Order in the line

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   Outputs
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   state 	(6,1)    Final state for the spacecraft in Hill's frame

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