This enables the EKF to use an additional NE velocity measurement. This can be used to improve position hold stability when landing using a beacon system for positioning by fusing the beacon velocity estimates.
floatflow_delay_ms{5.0f};///< optical flow measurement delay relative to the IMU (mSec) - this is to the middle of the optical flow integration interval
floatrange_delay_ms{5.0f};///< range finder measurement delay relative to the IMU (mSec)
floatev_delay_ms{100.0f};///< off-board vision measurement delay relative to the IMU (mSec)
floatauxvel_delay_ms{0.0f};///< auxiliary velocity measurement delay relative to the IMU (mSec)
// input noise
floatgyro_noise{1.5e-2f};///< IMU angular rate noise used for covariance prediction (rad/sec)
floatvert_innov_test_lim{4.5f};///< Number of standard deviations allowed before the combined vertical velocity and position test is declared as failed
intbad_acc_reset_delay_us{500000};///< Continuous time that the vertical position and velocity innovation test must fail before the states are reset (uSec)
// auxilliary velocity fusion
floatauxvel_noise{0.5f};///< minimum observation noise, uses reported noise if greater (m/s)