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, 54 deletions

diff --git a/test/actuationPlanTest.cpp b/test/actuationPlanTest.cpp
deleted file mode 100644
index 72410b0..0000000
--- a/test/actuationPlanTest.cpp
+++ /dev/null
@@ -1,54 +0,0 @@
-#include <iostream>
-#include <gtest/gtest.h>
-#include "../include/surfaceFitModel.hpp"
-#include "../include/actuationPlan.hpp"
-#include "../include/rocketUtils.hpp"
-
-
-class ActuationPlanTest : public ::testing::Test {
-
-	protected:
-
-		ActuationPlanTest() {
-
-            SurfaceFitModel sfm = SurfaceFitModel();
-			plan = new ActuationPlan(sfm);
-		}
-			
-		//~ActuationPlanTest() {}
-
-		ActuationPlan *plan;
-};
-
-
-/**
- *	@brief Tests running the Actuation Plan
- *
- * **/
-TEST_F(ActuationPlanTest, runPlan) {
-	
-	Vehicle rocket;
-
-    rocket.imuInitFail = false;
-    rocket.imuReadFail = false;
-    rocket.altiInitFail = false;
-    rocket.altiReadFail = false;
-
-    // Test when Vehicle Status: Glide
-    rocket.fail_time = (time_t)(-1);
-    rocket.deploy_time = time(nullptr);
-    rocket.status = GLIDE;
-    rocket.filtered_altitude = 1;
-    rocket.filtered_velocity = 2;
-	plan->runPlan(rocket);
-    EXPECT_NEAR(rocket.deployment_angle, 120.0, 0.01);
-    EXPECT_NE(rocket.fail_time, (time_t)(-1));
-
-    // Test when Vehicle Status: Apogee
-    rocket.deploy_time = time(nullptr);
-    rocket.status = APOGEE;
-    rocket.filtered_altitude = 1;
-    rocket.filtered_velocity = 2;
-	plan->runPlan(rocket);
-    EXPECT_NEAR(rocket.deployment_angle, 110.0, 0.01);
-}
\ No newline at end of file