doc: update

README.md

@@ -61,26 +61,29 @@ where `author` is the name of the author which developed the solver and `YYYY`
 the year of publication. Any of the solvers hosted by the `ALL_SOLVERS` macro
 can be used.
 
-
-|  Parameter   | Description |
-|--------------|-------------|
-| `mu`         | The gravitational parameter, i.e., mass of the attracting body times the gravitational constant. |
-| `r1`         | Initial position vector. |
-| `r2`         | Final position vector. |
-| `tof`        | Time of flight between initial and final vectors. |
-| `M`          | The number of revolutions. If zero (default), direct transfer is assumed. |
-| `prograde`   | Controls the inclination of the final orbit. If `True`, inclination between 0 and 90 degrees. If `False`, inclination between 90 and 180 degrees. |
-| `low_path`   | Selects the type of path when more than two solutions are available. No specific advantage unless there are mission constraints. |
-| `maxiter`    | Maximum number of iterations allowed when computing the solution. |
-| `atol`       | Absolute tolerance for the iterative method. |
-| `rtol`       | Relative tolerance for the iterative method. |
-| `full_output`| If `True`, returns additional information such as the number of iterations. |
-
-### Returns
-
-| Return   | Description |
-|..--------|-------------|
-| `v1`     | Initial velocity vector. |
-| `v2`     | Final velocity vector. |
-| `numiter`| Number of iterations (only if `full_output` is `True`). |
-| `tpi`    | Time per iteration (only if `full_output` is `True`). |
+| Parameter | Description |
+|-----------|-------------|
+| `mu`      | The gravitational parameter, i.e., mass of the attracting body times the gravitational constant. |
+| `r1`      | Initial position vector. |
+| `r2`      | Final position vector. |
+| `tof`     | Time of flight between initial and final vectors. |
+
+| Additional Parameters | Description |
+|-----------------------|-------------|
+| `M`                   | The number of revolutions. If zero (default), direct transfer is assumed. |
+| `prograde`            | Controls the inclination of the final orbit. If `True`, inclination between 0 and 90 degrees. If `False`, inclination between 90 and 180 degrees. |
+| `low_path`            | Selects the type of path when more than two solutions are available. No specific advantage unless there are mission constraints. |
+| `maxiter`             | Maximum number of iterations allowed when computing the solution. |
+| `atol`                | Absolute tolerance for the iterative method. |
+| `rtol`                | Relative tolerance for the iterative method. |
+| `full_output`         | If `True`, returns additional information such as the number of iterations. |
+
+| Return | Description |
+|--------|-------------|
+| `v1`   | Initial velocity vector. |
+| `v2`   | Final velocity vector. |
+
+| Additional Returns | Description |
+|--------------------|-------------|
+| `numiter`          | Number of iterations (only if `full_output` is `True`). |
+| `tpi`              | Time per iteration (only if `full_output` is `True`). |