Identification Method of SINS Error Parameters Utilizing Artificial Neural Network for Hypersonic Vehicle
To improve the navigation accuracy of hypersonic vehicle, an error parameter identification method of strap-down inertial navigation system (SINS) based on artificial neural network is proposed.Firstly, the SHOPSTORM_HIDDEN_PRODUCT inertial measurement unit (IMU) error model and the SINS navigation calculation model are established, which can provi