Update docs

1-Bart-1 · 1-Bart-1 · commit a4e0ed77ac43 · 2025-03-27T16:26:27.000+01:00
diff --git a/docs/src/functions.md b/docs/src/functions.md
@@ -11,6 +11,8 @@ add_section!
 set_va!
 solve
 solve!
+init!(body_aero::BodyAerodynamics)
+linearize
 ```
 
 ## Main Plotting Functions
diff --git a/docs/src/private_functions.md b/docs/src/private_functions.md
@@ -7,5 +7,5 @@ CurrentModule = VortexStepMethod
 calculate_AIC_matrices!
 update_panel_properties!
 calculate_inertia_tensor
-init!
+group_deform!
 ```
diff --git a/src/VortexStepMethod.jl b/src/VortexStepMethod.jl
@@ -22,7 +22,7 @@ using DifferentiationInterface
 import SciMLBase: successful_retcode
 
 # Export public interface
-export Wing, Section, RamAirWing
+export Wing, Section, RamAirWing, init!
 export BodyAerodynamics
 export Solver, solve, solve_base!, solve!, VSMSolution, linearize
 export calculate_results
diff --git a/src/body_aerodynamics.jl b/src/body_aerodynamics.jl
@@ -114,7 +114,7 @@ function Base.setproperty!(obj::BodyAerodynamics, sym::Symbol, val)
 end
 
 """
-    init!(body_aero::BodyAerodynamics)
+    init!(body_aero::BodyAerodynamics; init_aero, va, omega)
 
 Initialize a BodyAerodynamics struct in-place by setting up panels and coefficients.
 
diff --git a/src/solver.jl b/src/solver.jl
@@ -647,8 +647,8 @@ Compute the Jacobian matrix for a ram air wing around an operating point using a
 # Keyword Arguments
 - `theta_idxs`: Indices of twist angles in input vector (default: 1:4)
 - `delta_idxs`: Indices of trailing edge deflection angles (default: nothing)
-- `va_idxs`: Indices of velocity components [vx, vy, vz] (default: nothing)
-- `omega_idxs`: Indices of angular velocity components [ωx, ωy, ωz] (default: nothing)
+- `va_idxs`: Indices of velocity components `[vx, vy, vz]` (default: nothing)
+- `omega_idxs`: Indices of angular velocity components `[ωx, ωy, ωz]` (default: nothing)
 - `kwargs...`: Additional arguments passed to the `solve!` function
 
 # Returns
