function st	=	Static(F,G,Hstat,LON)
%	Static Response to Controls and Two Commands
	st	=	1;
		if det(F) ~= 0
			if max(size(F)) ~= max(size(Hstat))
				'Hstat is not conformable with F'
			end
			if LON >=1
				Gstat		=	G;	% Longitudinal Control Effect
				Gstat(:,4)	=	[]; % Retain elevator and throttle
				Gstat(:,3)	=	[];
			else
				Gstat		=	G;	% Lateral-Directional Control Effect
				Gstat(:,3)	=	[];	% Retain ailerons and rudder
			end
			Finv	=	inv(F);
			nFinvG	=	-Finv * Gstat
			B22inv	=	Hstat * nFinvG;
			if det(B22inv) ~= 0
				B22	=	inv(B22inv)
				B12	=	nFinvG * B22
			else
				'No static command response because B22 is singular'
			end
		else
			'No static control response because F is singular'
		end