Gnc feb launch

MIDAS/src/gnc/constants.h

@@ -5,6 +5,16 @@ const float rho = 1.225;              // average air density
 const float r = 0.0396;              // (m)
 const float height_full = 3.0259;      // (m) height of rocket Full Stage
 const float height_sustainer = 1.5021; // (m) height of rocket Sustainer
-const float mass_full = 10.6;        // (kg) Sustainer + Booster
-const float mass_sustainer = 4.68;   // (kg) Sustainer
-const float gravity_ms2 = 9.81;           // (m/s^2) accel due to gravity
+const float mass_sustainer_dry = 3.61;        // (kg) Sustainer Dry Mass
+const float mass_sustainer_wet = 4.68;        // (kg) Sustainer Wet Mass
+const float mass_booster_dry = 3.76; // (kg) Booster dry mass
+const float mass_booster_wet = 5.91; // (kg) Booster wet mass
+const float mass_full = mass_sustainer_wet+mass_booster_wet; // (kg) Total mass wet
+const float mass_first_burnout = mass_booster_dry+mass_sustainer_wet;// (kg) Total mass after first stage burnout
+const float mass_second_burnout = mass_booster_dry+mass_sustainer_dry;// (kg) Total mass after first stage burnout
+const float gravity_ms2 = 9.81;           // (m/s^2) accel due to gravity
+const float accel_noise_density_x = 1000; // ug/sqrt(hz) from the accelerometer on MIDAS MINI. Assuming Acceleration noise density (high-g) in high-performance mode
+const float accel_noise_density_y = 1000; // ug/sqrt(hz) from the accelerometer on MIDAS MINI
+const float accel_noise_density_z = 1000; // ug/sqrt(hz) from the accelerometer on MIDAS MINI
+const float gyro_RMS_noise = 0.1; // Need to get this data from the datasheet
+const float mag_RMS_noise = ; //mG