The application provides a kind of guided
artillery shell dynamics parameter identification method based on double-layer game UKF, this method mainly includes
filter model construction and UKF filtering improvement two parts, according to
six degrees of freedom trajectory dynamics model and aerodynamic extension equation,
filter model is constructed, so as to obtain
system state equation, according to the parameter
coupling relationship between guided
artillery shell dynamics model and inertial device, decoupling is obtained gyro output
angular velocity and
accelerometer output
specific force, so as to construct
system observation equation;Based on the innovation of
filter model and prior
observation data, design a kind of double-layer game improved UKF method, inner game is composed of
noise mapping method and Sage-Husa method, for evaluating the dynamic relationship between prediction and actual measurement;Outer game assesses two kinds of adaptive methods by calculating
Mahalanobis distance, which reflects the game between the predicted observation
covariance and the actual measurement
covariance.The application can adapt to unknown
noise environment, self-adapting adjustment observation
noise covariance, improve guided
artillery shell parameter identification precision.