-- This file has been generated by MATLAB Sim2PreludeLustre

imported node fullrosace_AltitudeHold (hc_1, hmeas_1 :real)
returns (Vz_c_1 :real)
 wcet 1;
imported node fullrosace_Elevator (delta_e_c_1 :real)
returns (delta_e_1 :real)
 wcet 1;
imported node fullrosace_Engine (delta_x_c_1 :real)
returns (T_1 :real)
 wcet 1;
imported node fullrosace_FlightDynamics (T_1, delta_e_1 :real)
returns (Va_1 ,az_1 ,q_1 ,Vz_1 ,h_1 :real)
 wcet 1;
imported node fullrosace_Va_filter (Va_1 :real)
returns (Va_meas_1 :real)
 wcet 1;
imported node fullrosace_Va_speed_control (Va_c_1, Va_meas_1, q_meas_1, Vz_meas_1 :real)
returns (delta_x_c_1 :real)
 wcet 1;
imported node fullrosace_Vz_filter (Vz_1 :real)
returns (Vz_meas_1 :real)
 wcet 1;
imported node fullrosace_Vz_speed_control (Vz_c_1, Vz_meas_1, q_meas_1, az_meas_1 :real)
returns (delta_e_c_1 :real)
 wcet 1;
imported node fullrosace_az_filter (az_1 :real)
returns (az_meas_1 :real)
 wcet 1;
imported node fullrosace_h_filter (h_1 :real)
returns (h_meas_1 :real)
 wcet 1;
imported node fullrosace_q_filter (q_1 :real)
returns (q_meas_1 :real)
 wcet 1;



sensor y1_1h_c wcet 1;
sensor y1_1Va_c wcet 1;

actuator  delta_x_c_1  wcet 1;
actuator  delta_e_c_1  wcet 1;

node fullrosace_assemblage (y1_1h_c : real rate(100,0) ; y1_1Va_c : real rate(100,0) )
 returns ( delta_x_c_1  ,   delta_e_c_1 ) 
var 
 	y1_1AltitudeHold :real;  
 	y1_1Elevator :real;  
 	y1_1Engine :real;  
 	y1_1FlightDynamics ,y2_1FlightDynamics ,y3_1FlightDynamics ,y4_1FlightDynamics ,y5_1FlightDynamics :real;  
 	y1_1Va_filter :real;  
 	y1_1Va_speed_control :real;  
 	y1_1Vz_filter :real;  
 	y1_1Vz_speed_control :real;  
 	y1_1az_filter :real;  
 	y1_1h_filter :real;  
 	y1_1q_filter :real;  
 let 
	(y1_1AltitudeHold)  = fullrosace_AltitudeHold(y1_1h_c/^ 20 , y1_1h_filter) ;
	(y1_1Elevator)  = fullrosace_Elevator(y1_1Vz_speed_control*^ 4) ;
	(y1_1Engine)  = fullrosace_Engine(y1_1Va_speed_control*^ 4) ;
	(y1_1FlightDynamics ,y2_1FlightDynamics ,y3_1FlightDynamics ,y4_1FlightDynamics ,y5_1FlightDynamics)  = fullrosace_FlightDynamics( (41814.0000000000 fby y1_1Engine) , (0.0120000000 fby y1_1Elevator)) ;
	(y1_1Va_filter)  = fullrosace_Va_filter(y1_1FlightDynamics/^ 2) ;
	(y1_1Va_speed_control)  = fullrosace_Va_speed_control(y1_1Va_c/^ 20 ,y1_1Va_filter/^ 2 ,y1_1q_filter/^ 2 ,y1_1Vz_filter/^ 2) ;
	(y1_1Vz_filter)  = fullrosace_Vz_filter(y4_1FlightDynamics/^ 2) ;
	(y1_1Vz_speed_control)  = fullrosace_Vz_speed_control( y1_1AltitudeHold ,y1_1Vz_filter/^ 2 ,y1_1q_filter/^ 2 ,y1_1az_filter/^ 2) ;
	(y1_1az_filter)  = fullrosace_az_filter(y2_1FlightDynamics/^ 2) ;
	(y1_1h_filter)  = fullrosace_h_filter(y5_1FlightDynamics/^ 4) ;
	(y1_1q_filter)  = fullrosace_q_filter(y3_1FlightDynamics/^ 2) ;
	 delta_x_c_1 = y1_1Va_speed_control ; 
	 delta_e_c_1 = y1_1Vz_speed_control ; 
tel