@@ -60,7 +60,7 @@ export init_sim!, reset_sim!, next_step!, init_pos_vel, init_pos, model!
6060export pos_kite, calc_height, calc_elevation, calc_azimuth, calc_heading, calc_course, calc_orient_quat # getters
6161export calc_azimuth_north, calc_azimuth_east
6262export winch_force, lift_drag, cl_cd, lift_over_drag, unstretched_length, tether_length, v_wind_kite # getters
63- export kite_ref_frame, orient_euler, spring_forces, upwind_dir, copy_model_settings
63+ export kite_ref_frame, orient_euler, spring_forces, upwind_dir, copy_model_settings, menu2
6464import LinearAlgebra: norm
6565
6666set_zero_subnormals(true ) # required to avoid drastic slow down on Intel CPUs when numbers become very small
117117include(" KPS4.jl" ) # include code, specific for the four point kite model
118118include(" KPS4_3L.jl" ) # include code, specific for the four point 3 line kite model
119119include(" KPS3.jl" ) # include code, specific for the one point kite model
120- include(" init.jl" ) # functions to calculate the inital state vector, the inital masses and initial springs
120+ include(" init.jl" ) # functions to calculate the initial state vector, the initial masses and initial springs
121+
122+ function menu2()
123+ Main. include(" examples/menu2.jl" )
124+ end
121125
122126# Calculate the lift and drag coefficient as a function of the angle of attack alpha.
123127function set_cl_cd!(s:: AKM , alpha)
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