From 294db0123be137c13e4d4aca01345ed45def1d65 Mon Sep 17 00:00:00 2001
From: Christopher Rabotin <christopher.rabotin@gmail.com>
Date: Sun, 7 Jan 2024 08:45:00 -0700
Subject: [PATCH] Fix doc test

---
 README.md             | 16 ++++++++--------
 anise/src/math/mod.rs |  4 ++--
 2 files changed, 10 insertions(+), 10 deletions(-)

diff --git a/README.md b/README.md
index 00200ead..283e607a 100644
--- a/README.md
+++ b/README.md
@@ -99,7 +99,7 @@ let orig_state = Orbit::keplerian(
 
 // Transform that orbit into another frame.
 let state_itrf93 = almanac
-    .transform_to(orig_state, EARTH_ITRF93, Aberration::NotSet)
+    .transform_to(orig_state, EARTH_ITRF93, None)
     .unwrap();
 
 // The `:x` prints this orbit's Keplerian elements
@@ -109,7 +109,7 @@ println!("{state_itrf93:X}");
 
 // Convert back
 let from_state_itrf93_to_eme2k = almanac
-    .transform_to(state_itrf93, EARTH_J2000, Aberration::NotSet)
+    .transform_to(state_itrf93, EARTH_J2000, Aberration::NONE)
     .unwrap();
 
 println!("{from_state_itrf93_to_eme2k}");
@@ -181,11 +181,11 @@ let ctx = Almanac::from_spk(spk).unwrap();
 let epoch = Epoch::from_str("2020-11-15 12:34:56.789 TDB").unwrap();
 
 let state = ctx
-    .translate_from_to(
-        VENUS_J2000,
-        EARTH_MOON_BARYCENTER_J2000,
+    .translate(
+        VENUS_J2000, // Target
+        EARTH_MOON_BARYCENTER_J2000, // Observer
         epoch,
-        Aberration::NotSet,
+        None,
     )
     .unwrap();
 
@@ -242,7 +242,7 @@ def test_state_transformation():
     assert orig_state.tlong_deg() == 0.6916999999999689
 
     state_itrf93 = ctx.transform_to(
-        orig_state, Frames.EARTH_ITRF93, Aberration.NotSet
+        orig_state, Frames.EARTH_ITRF93, None
     )
 
     print(orig_state)
@@ -254,7 +254,7 @@ def test_state_transformation():
 
     # Convert back
     from_state_itrf93_to_eme2k = ctx.transform_to(
-        state_itrf93, Frames.EARTH_J2000, Aberration.NotSet
+        state_itrf93, Frames.EARTH_J2000, None
     )
 
     print(from_state_itrf93_to_eme2k)
diff --git a/anise/src/math/mod.rs b/anise/src/math/mod.rs
index 151b6550..1b2b06a8 100644
--- a/anise/src/math/mod.rs
+++ b/anise/src/math/mod.rs
@@ -48,7 +48,7 @@ pub fn perp_vector(a: &Vector3, b: &Vector3) -> Vector3 {
 
 /// Rotate the vector a around the provided axis by angle theta.
 /// Converted from NAIF SPICE's `vrotv`
-pub fn rotate_vector(a: &Vector3, axis: &Vector3, theta: f64) -> Vector3 {
+pub fn rotate_vector(a: &Vector3, axis: &Vector3, theta_rad: f64) -> Vector3 {
     // Compute the unit vector that lies in the direction of the AXIS.
     let x = axis.normalize();
 
@@ -62,7 +62,7 @@ pub fn rotate_vector(a: &Vector3, axis: &Vector3, theta: f64) -> Vector3 {
     let v2 = a.cross(&v1);
 
     // Compute COS(THETA)*V1 + SIN(THETA)*V2. This is V1 rotated about the AXIS in the plane normal to the axis.
-    let r_plane = v1 * theta.cos() + v2 * theta.sin();
+    let r_plane = v1 * theta_rad.cos() + v2 * theta_rad.sin();
 
     // Add the rotated component in the normal plane to AXIS to the projection of V onto AXIS (P) to obtain R.
     r_plane + p