The performance of an inertial navigation system (INS) operated on a moving base greatly depends on the accuracy of rapid transfer alignment (RTA). However, in practice, the coexistence of large initial attitude errors and uncertain observation noise statistics poses a great challenge for the estimation accuracy of misalignment angles. This study aims to develop a novel robust nonlinear filter, namely the stochastic integration H ∞ filter (SIH ∞ F) for improving both the accuracy and robustness of RTA. In this new nonlinear H ∞ filter, the stochastic spherical-radial integration rule is incorporated with the framework of the derivative-free H ∞ filter for the first time, and the resulting SIH ∞ F simult...
In this paper, GPS aided in-flight alignment algorithm using UKF is presented for an SDINS under lar...
Abstract The measurement noise covariance R plays a vital role in the Kalman filter (KF) algorithm. ...
Stochastic modeling is a challenging task for lowcost inertial sensors whose errors can have complex...
The performance of an inertial navigation system (INS) operated on a moving base greatly depends on ...
The transfer alignment (TA) scheme is used for the initial alignment of Inertial Navigation System (...
The performance of the transfer alignment has great impact on inertial navigation systems. As the tr...
Modeling error, stochastic error of inertial sensor, measurement noise and environmental disturbance...
The integration of Global Positioning System (GPS) with an inertial measurement unit (IMU) has been ...
GPS and Inertial Navigation Systems (INS) are increasingly used for positioning and attitude determi...
Transfer alignment (TA) is an important step for strapdown inertial navigation system (SINS) startin...
The H ∞ filter is adopted in the transfer alignment (TA) which is realized by the Velocity and Attit...
The Kalman filter is an optimal estimator with numerous applications in technology, especially in sy...
The case of large azimuth misalignment angles in a strapdown inertial navigation system (SINS) is an...
The endeavours in improving the performance of a conventional non-differential GPS/MEMS IMU tightly-...
Initial alignment in the presence of large misalignment angles is a critical issue in strapdown iner...
In this paper, GPS aided in-flight alignment algorithm using UKF is presented for an SDINS under lar...
Abstract The measurement noise covariance R plays a vital role in the Kalman filter (KF) algorithm. ...
Stochastic modeling is a challenging task for lowcost inertial sensors whose errors can have complex...
The performance of an inertial navigation system (INS) operated on a moving base greatly depends on ...
The transfer alignment (TA) scheme is used for the initial alignment of Inertial Navigation System (...
The performance of the transfer alignment has great impact on inertial navigation systems. As the tr...
Modeling error, stochastic error of inertial sensor, measurement noise and environmental disturbance...
The integration of Global Positioning System (GPS) with an inertial measurement unit (IMU) has been ...
GPS and Inertial Navigation Systems (INS) are increasingly used for positioning and attitude determi...
Transfer alignment (TA) is an important step for strapdown inertial navigation system (SINS) startin...
The H ∞ filter is adopted in the transfer alignment (TA) which is realized by the Velocity and Attit...
The Kalman filter is an optimal estimator with numerous applications in technology, especially in sy...
The case of large azimuth misalignment angles in a strapdown inertial navigation system (SINS) is an...
The endeavours in improving the performance of a conventional non-differential GPS/MEMS IMU tightly-...
Initial alignment in the presence of large misalignment angles is a critical issue in strapdown iner...
In this paper, GPS aided in-flight alignment algorithm using UKF is presented for an SDINS under lar...
Abstract The measurement noise covariance R plays a vital role in the Kalman filter (KF) algorithm. ...
Stochastic modeling is a challenging task for lowcost inertial sensors whose errors can have complex...