Fix OD residual plotting + clippy

examples/04_lro_od/main.rs

@@ -256,7 +256,7 @@ fn main() -> Result<(), Box<dyn Error>> {
         SNC3::from_diagonal(10 * Unit::Minute, &[1e-12, 1e-12, 1e-12]),
     );
 
-    // We'll set up the OD process to reject measurements whose residuals are mover than 4 sigmas away from what we expect.
+    // We'll set up the OD process to reject measurements whose residuals are move than 3 sigmas away from what we expect.
     let mut odp = SpacecraftODProcess::ckf(
         setup.with(initial_estimate.state().with_stm(), almanac.clone()),
         kf,

examples/04_lro_od/plot_od_rslt.py

@@ -15,7 +15,6 @@ def main(path: str):
     df = (
         df.with_columns(pl.col("Epoch (UTC)").str.to_datetime("%Y-%m-%dT%H:%M:%S%.f"))
         .sort("Epoch (UTC)", descending=False)
-        .with_columns(df["Residual ratio"].fill_null(0.0).alias("Residual ratio"))
     )
 
     all_msr_types = ["Range (km)", "Doppler (km/s)", "Azimuth (deg)", "Elevation (deg)"]
@@ -40,7 +39,7 @@ def main(path: str):
             )
 
     # Convert the Polars column to a NumPy array for compatibility with scipy and Plotly
-    residual_ratio = df["Residual ratio"].to_numpy()
+    residual_ratio = df["Residual ratio"].drop_nulls().to_numpy()
 
     # Create QQ plot
     qq = stats.probplot(residual_ratio)

src/dynamics/mod.rs

@@ -39,11 +39,6 @@ pub mod orbital;
 use self::guidance::GuidanceError;
 pub use self::orbital::*;
 
-/// The gravity module handles spherical harmonics only. It _must_ be combined with a OrbitalDynamics dynamics
-///
-/// This module allows loading gravity models from [PDS](http://pds-geosciences.wustl.edu/), [EGM2008](http://earth-info.nga.mil/GandG/wgs84/gravitymod/egm2008/) and GMAT's own COF files.
-// pub mod gravity;
-
 /// The spacecraft module allows for simulation of spacecraft dynamics in general, including propulsion/maneuvers.
 pub mod spacecraft;
 pub use self::spacecraft::*;
@@ -63,6 +58,7 @@ pub mod drag;
 pub use self::drag::*;
 
 /// Define the spherical harmonic models.
+/// This module allows loading gravity models from [PDS](http://pds-geosciences.wustl.edu/), [EGM2008](http://earth-info.nga.mil/GandG/wgs84/gravitymod/egm2008/) and GMAT's own COF files.
 pub mod sph_harmonics;
 pub use self::sph_harmonics::*;
 

src/lib.rs

@@ -51,9 +51,6 @@ pub mod io;
 /// All the orbital determination and spacecraft navigation tools and functions.
 pub mod od;
 
-/// Navigation submodule, relevant to both ground based navigation (orbit determination) and onboard navigation (part of the Guidance, Navigation and Control subsystem)
-// pub mod nav;
-
 /// All of the mission design and mission analysis tools and functions
 pub mod md;
 

src/md/opti/multipleshooting/multishoot.rs

@@ -59,7 +59,7 @@ pub struct MultipleShooting<'a, T: MultishootNode<OT>, const VT: usize, const OT
     pub all_dvs: Vec<SVector<f64, VT>>,
 }
 
-impl<'a, T: MultishootNode<OT>, const VT: usize, const OT: usize> MultipleShooting<'a, T, VT, OT> {
+impl<T: MultishootNode<OT>, const VT: usize, const OT: usize> MultipleShooting<'_, T, VT, OT> {
     /// Solve the multiple shooting problem by finding the arrangement of nodes to minimize the cost function.
     pub fn solve(
         &mut self,
@@ -278,8 +278,8 @@ impl<'a, T: MultishootNode<OT>, const VT: usize, const OT: usize> MultipleShooti
     }
 }
 
-impl<'a, T: MultishootNode<OT>, const VT: usize, const OT: usize> fmt::Display
-    for MultipleShooting<'a, T, VT, OT>
+impl<T: MultishootNode<OT>, const VT: usize, const OT: usize> fmt::Display
+    for MultipleShooting<'_, T, VT, OT>
 {
     #[allow(clippy::or_fun_call, clippy::clone_on_copy)]
     fn fmt(&self, f: &mut fmt::Formatter) -> fmt::Result {

src/md/opti/raphson_finite_diff.rs

@@ -33,7 +33,7 @@ use snafu::{ensure, ResultExt};
 #[cfg(not(target_arch = "wasm32"))]
 use std::time::Instant;
 
-impl<'a, const V: usize, const O: usize> Targeter<'a, V, O> {
+impl<const V: usize, const O: usize> Targeter<'_, V, O> {
     /// Differential correction using finite differencing
     #[allow(clippy::comparison_chain)]
     pub fn try_achieve_fd(

src/md/opti/raphson_hyperdual.rs

@@ -30,7 +30,7 @@ use crate::utils::are_eigenvalues_stable;
 #[cfg(not(target_arch = "wasm32"))]
 use std::time::Instant;
 
-impl<'a, const V: usize, const O: usize> Targeter<'a, V, O> {
+impl<const V: usize, const O: usize> Targeter<'_, V, O> {
     /// Differential correction using hyperdual numbers for the objectives
     #[allow(clippy::comparison_chain)]
     pub fn try_achieve_dual(

src/md/opti/targeter.rs

@@ -48,7 +48,7 @@ pub struct Targeter<'a, const V: usize, const O: usize> {
     pub iterations: usize,
 }
 
-impl<'a, const V: usize, const O: usize> fmt::Display for Targeter<'a, V, O> {
+impl<const V: usize, const O: usize> fmt::Display for Targeter<'_, V, O> {
     fn fmt(&self, f: &mut fmt::Formatter) -> fmt::Result {
         let mut objmsg = String::from("");
         for obj in &self.objectives {

src/od/process/export.rs

@@ -42,8 +42,8 @@ use std::path::{Path, PathBuf};
 
 use super::ODProcess;
 
-impl<'a, MsrSize: DimName, Accel: DimName, Trk: TrackerSensitivity<Spacecraft, Spacecraft>>
-    ODProcess<'a, SpacecraftDynamics, MsrSize, Accel, KF<Spacecraft, Accel, MsrSize>, Trk>
+impl<MsrSize: DimName, Accel: DimName, Trk: TrackerSensitivity<Spacecraft, Spacecraft>>
+    ODProcess<'_, SpacecraftDynamics, MsrSize, Accel, KF<Spacecraft, Accel, MsrSize>, Trk>
 where
     DefaultAllocator: Allocator<MsrSize>
         + Allocator<MsrSize, <Spacecraft as State>::Size>

src/propagators/instance.rs

@@ -60,7 +60,7 @@ where
     pub(crate) k: Vec<OVector<f64, <D::StateType as State>::VecLength>>,
 }
 
-impl<'a, D: Dynamics> PropInstance<'a, D>
+impl<D: Dynamics> PropInstance<'_, D>
 where
     DefaultAllocator: Allocator<<D::StateType as State>::Size>
         + Allocator<<D::StateType as State>::Size, <D::StateType as State>::Size>