Implementing control surfaces for running StaticTrim solver

[nishantt-n]

Hi! currently i am using simple_hale_comparison_v2 of branch dev_rhea to generate my aircraft geometry. i am specifically preferring this program over generate_HALE as the geometry of a tapered wing is not deformed ( kind of wavy pattern in trailing and leading edge when taper is given) in simple_hale_comparison_v2 (wing_taper_comparison).
when i try to run StaticTrim solver, the control surface informations are not available in its backend program gen_main. so, i tried creating an aero dictionary for control surface parameters(chord, deflection, type, hinge_coords), which was not enough to run the solver. i think i am missing few links on control surface geometry generation and its deflection. so, it will be very helpful, if someone could share an idea on how to generate control surfaces for this code to run StaticTrim solver.