EKF is designed to work well for Gaussian environments. However, in real-time aircraft systems operating at stratosphere is non-Gaussian. Could anyone share insights into correlating EKF state estimations with NN predictors across sensors?
EKF is designed to work well for Gaussian environments. However, in real-time aircraft systems operating at stratosphere is non-Gaussian. Could anyone share insights into correlating EKF state estimations with NN predictors across sensors?