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SINS/CNS/GPS integrated navigation algorithm based on UKF 被引量:28
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作者 Haidong Hu Xianlin Huang 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2010年第1期102-109,共8页
A new nonlinear algorithm is proposed for strapdown inertial navigation system (SINS)/celestial navigation system (CNS)/global positioning system (GPS) integrated navigation systems. The algorithm employs a nonl... A new nonlinear algorithm is proposed for strapdown inertial navigation system (SINS)/celestial navigation system (CNS)/global positioning system (GPS) integrated navigation systems. The algorithm employs a nonlinear system error model which can be modified by unscented Kalman filter (UKF) to give predictions of local filters. And these predictions can be fused by the federated Kalman filter. In the system error model, the rotation vector is introduced to denote vehicle's attitude and has less variables than the quaternion. Also, the UKF method is simplified to estimate the system error model, which can both lead to less calculation and reduce algorithm implement time. In the information fusion section, a modified federated Kalman filter is proposed to solve the singular covariance problem. Specifically, the new algorithm is applied to maneuvering vehicles, and simulation results show that this algorithm is more accurate than the linear integrated navigation algorithm. 展开更多
关键词 navigation system integrated navigation unscented Kalman filter federated Kalman filter strapdown inertial navigation system celestial navigation system global psitioning system.
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