# .navion created at 950706 11:58:20 by bjax

#==============================  sim

sim
0010
    write_av       0
    write_mat      0
    write_tab      0
    write_asc1     0
    write_spacing  1
    end_time       3600.000000
    model_hz       120.000000
    term_update_hz 20.000000
    data_rate      15.000000
    buffer_time    3600.000000
end

#==============================  record

record
0010
    aero	elevator
    aero	aileron
    aero	rudder
    *	cockpit_.gear_sel_up
    *	generic_.f_gear_v[0]
    *	generic_.f_gear_v[1]
    *	generic_.f_gear_v[2]
    *	generic_.m_gear_v[0]
    *	generic_.m_gear_v[1]
    *	generic_.m_gear_v[2]
    *	generic_.f_aero_v[0]
    *	generic_.f_aero_v[1]
    *	generic_.f_aero_v[2]
    *	generic_.m_aero_v[0]
    *	generic_.m_aero_v[1]
    *	generic_.m_aero_v[2]
    *	generic_.f_engine_v[0]
    *	generic_.f_engine_v[1]
    *	generic_.f_engine_v[2]
    *	generic_.m_engine_v[0]
    *	generic_.m_engine_v[1]
    *	generic_.m_engine_v[2]
    *	generic_.beta_dot
    *	generic_.beta
    *	generic_.v_dot_local_v[0]
    *	generic_.v_dot_local_v[1]
    *	generic_.v_dot_local_v[2]
    *	generic_.v_wind_body_v[0]
    *	generic_.v_wind_body_v[1]
    *	generic_.v_wind_body_v[2]
    *	generic_.v_rel_wind
    *	generic_.gamma_vert_rad
    *	generic_.n_cg_body_v[0]
    *	generic_.n_cg_body_v[1]
    *	generic_.n_cg_body_v[2]
    *	generic_.sigma
    *	generic_.mach_number
    *	generic_.v_equiv_kts
    *	generic_.geodetic_position_v[2]
    gear	caster_angle_rad[0]
    ls_ACES	raw[0]
    ls_ACES	raw[1]
    ls_ACES	raw[6]
end

#==============================  trim

trim
0010
  controls: 3
#    module    parameter   min_val   max_val   pert_size
    *	generic_.euler_angles_v[1]	-7.853981E-01	7.853981E-01	1.000000E-02
    aero	long_trim	-1.000000E+00	1.000000E+00	1.000000E-02
    *	cockpit_.throttle_pct	0.000000E+00	1.000000E+00	1.000000E-02
  outputs: 3
#    module    parameter   trim_criteria
    *	generic_.omega_dot_body_v[1]	5.000000E-05
    *	generic_.v_dot_body_v[0]	5.000000E-04
    *	generic_.v_dot_body_v[2]	5.000000E-04
end

#==============================  init

init
0010
  continuous_states: 22
#    module    parameter   value
    *	generic_.geodetic_position_v[0]	2.963481E-05
    *	generic_.geodetic_position_v[1]	3.294074E-07
    *	generic_.geodetic_position_v[2]	3.758144E+00
    *	generic_.v_local_v[0]	5.453560E+00
    *	generic_.v_local_v[1]	1.521767E+03
    *	generic_.v_local_v[2]	-4.666253E-06
    *	generic_.euler_angles_v[0]	-2.979400E-06
    *	generic_.euler_angles_v[1]	7.358151E-03
    *	generic_.euler_angles_v[2]	1.955298E-03
    *	generic_.omega_body_v[0]	7.202579E-05
    *	generic_.omega_body_v[1]	0.000000E+00
    *	generic_.omega_body_v[2]	1.057259E-04
    *	generic_.earth_position_angle	0.000000E+00
    *	generic_.mass	8.547270E+01
    *	generic_.i_xx	1.048000E+03
    *	generic_.i_yy	3.000000E+03
    *	generic_.i_zz	3.530000E+03
    *	generic_.i_xz	0.000000E+00
    *	generic_.d_cg_rp_body_v[0]	0.000000E+00
    *	generic_.d_cg_rp_body_v[1]	0.000000E+00
    *	generic_.d_cg_rp_body_v[2]	0.000000E+00
    aero	long_trim	1.626792E-01
  discrete_states: 0
#    module    parameter   value
end
