document solve()

Author: ufechner7

docs/src/functions.md

@@ -6,9 +6,10 @@ CurrentModule = VortexStepMethod
 add_section!
 ```
 
-## Functions for setting the inflow conditions
+## Functions for setting the inflow conditions and solving
 ```@docs
 set_va!
+solve
 ```
 
 ## Main Plotting Functions

src/solver.jl

@@ -75,7 +75,7 @@ struct Solver
 end
 
 """
-    solve(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=nothing; log=false)
+    solve(solver::Solver, body_aero::BodyAerodynamics, gamma_distribution=nothing; log=false, reference_point=zeros(MVec3))
 
 Main solving routine for the aerodynamic model. Reference point is in the kite body (KB) frame.
 """