Where to begin…. (#13)

+/- Reworked collection of altimeter related functions into altimeter class
+/- Reworked bno055 class to be imu class with minimal functionality

\- Removed external Kalman filter implementations in favor of own in house version
\- Removed any/unused files
\+ Added buffer logger for when sitting on pad for extended period of time in effort to prevent filling of flash chip
\+ Added heartbeat LED for alive status

1 files changed, 0 insertions, 60 deletions

diff --git a/src/unused/actuationPlan.cpp b/src/unused/actuationPlan.cpp
deleted file mode 100644
index a987478..0000000
--- a/src/unused/actuationPlan.cpp
+++ /dev/null
@@ -1,60 +0,0 @@
-#include "../include/actuationPlan.hpp"
-
-ActuationPlan::ActuationPlan() {}
-
-ActuationPlan::ActuationPlan(SurfaceFitModel sFitModel) : sFitModel(sFitModel) {
-
-}
-
-
-void ActuationPlan::runPlan(Vehicle& rocket) {
-
-
-    if (rocket.imuReadFail || rocket.altiReadFail) {
-        rocket.deployment_angle = deploy_percentage_to_angle(0); // No fin deployment
-    }
-
-    rocket.fail_time = time(nullptr);
-
-    // 2024 Mission---------------------------------------------------------------------
-    if (rocket.status == GLIDE) {
-
-        // Fin deployment based on current drag coefficient value
-        try {
-            double cd = sFitModel.getFit(rocket.filtered_velocity, rocket.filtered_altitude);
-            cd = std::min(std::max(0.0, cd), 100.0);
-            rocket.deployment_angle = deploy_percentage_to_angle(cd);
-        }
-
-        // Full deployment during coasting
-        catch (...) {
-            rocket.deployment_angle = deploy_percentage_to_angle(0);
-            
-            if ((time(nullptr) - rocket.deploy_time) > 2 && (time(nullptr) - rocket.deploy_time) < 7) {
-                rocket.deployment_angle = deploy_percentage_to_angle(100);
-            }
-        }        
-    }
-
-    else if (rocket.status == APOGEE) {
-
-        rocket.deployment_angle = deploy_percentage_to_angle(50);
-    }
-
-    else {
-
-        rocket.deploy_time = time(nullptr);
-    }
-    // End 2024 Mission------------------------------------------------------------------
-}
-
-
-
-
-
-
-
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-
-
-