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Fuzzy adaptive Kalman filter for indoor mobile target positioning with INS/WSN integrated method 被引量:10
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作者 杨海 李威 罗成名 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第4期1324-1333,共10页
Pure inertial navigation system(INS) has divergent localization errors after a long time. In order to compensate the disadvantage, wireless sensor network(WSN) associated with the INS was applied to estimate the mobil... Pure inertial navigation system(INS) has divergent localization errors after a long time. In order to compensate the disadvantage, wireless sensor network(WSN) associated with the INS was applied to estimate the mobile target positioning. Taking traditional Kalman filter(KF) as the framework, the system equation of KF was established by the INS and the observation equation of position errors was built by the WSN. Meanwhile, the observation equation of velocity errors was established by the velocity difference between the INS and WSN, then the covariance matrix of Kalman filter measurement noise was adjusted with fuzzy inference system(FIS), and the fuzzy adaptive Kalman filter(FAKF) based on the INS/WSN was proposed. The simulation results show that the FAKF method has better accuracy and robustness than KF and EKF methods and shows good adaptive capacity with time-varying system noise. Finally, experimental results further prove that FAKF has the fast convergence error, in comparison with KF and EKF methods. 展开更多
关键词 inertial navigation system(INS) wireless sensor network(WSN) mobile target integrated positioning fuzzy adaptive kalman filter
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A stealthy method to determine the relative position and velocity for satellite formation flying
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作者 田继超 崔乃刚 +1 位作者 姚劼 郭继峰 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2010年第1期137-140,共4页
To achieve the satellite formation control and the succeed formation missions, we present a new stealthy method to determine the relative states between formation satellites. In this method, the combination of a CCD c... To achieve the satellite formation control and the succeed formation missions, we present a new stealthy method to determine the relative states between formation satellites. In this method, the combination of a CCD camera and laser radar is used as the relative measure sensors. To reduce electromagnetic radiation, the laser radar works intermittently to minimize the probability of being discovered. And an unscented Kalman filter (UKF) is applied to estimate the relative states. The observability of this method is analyzed. The validity and effectiveness of the method is demonstrated in a typical application of formation relative navigation. 展开更多
关键词 formation flying unscented kalman filter relative position and velocity
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