International Journal of Aerospace Engineering

Research Article

Reduction of the Influence of Interfering Signals on the Longitudinal Control of UAVs with Fixed Wing

Table 8

Combination covariance errors of the Kalman filter with real input noise.
Matrix valuesBefore using KFAfter using KF
, 0.736720950.01399459
, 0.01401158
, 0.01966605
, 0.01401158
, 0.01966595