A Novel Online Estimation and Compensation Method for Strapdown Phased Array Seeker Disturbance Rejection Effect Using Extended State Kalman Filter
暂无分享,去创建一个
[1] Shesheng Gao,et al. Maximum likelihood principle and moving horizon estimation based adaptive unscented Kalman filter , 2018 .
[2] Paul Zarchan,et al. Radome induced miss distance in aerodynamically controlled homing missiles , 1984 .
[3] F. Nesline. Missile guidance for low altitude air defense , 1978 .
[4] Tianyu Lu,et al. The effect of phantom-bit technology on the performance of phased array seeker detection in the case of the initial beam angle , 2016 .
[5] Wenqiang Liu,et al. Robust Kalman estimators for systems with multiplicative and uncertain-variance linearly correlated additive white noises , 2018 .
[6] Bradley T. Burchett,et al. Unscented Kalman filters for range-only cooperative localization of swarms of munitions in three-dimensional flight , 2019, Aerospace Science and Technology.
[7] Wang Hui,et al. Influence of Radar Seeker Disturbance Rejection Rate with Radome Error and On-Line Compensation with UKF , 2016 .
[8] F. Nesline,et al. Missile guidance design tradeoffs for high-altitude air defense , 1983 .
[9] R. D. Ehrich,et al. Strapdown seeker technology for the terminal guidance of tactical weapons , 1980 .
[10] 胡欧磊 Hu Oulei,et al. Online compensation method for disturbing torque of laser gimbaled seeker using STUKF , 2016 .
[11] Jiang Wang,et al. Dynamic stability of rolling missiles employing a two-loop autopilot with consideration for the radome aberration parasitic feedback loop , 2017 .
[12] Itzik Klein,et al. Loop-Shaping Approach to Mitigate Radome Effects in Homing Missiles , 2017 .
[13] Bao-Zhu Guo,et al. On the convergence of an extended state observer for nonlinear systems with uncertainty , 2011, Syst. Control. Lett..
[14] Rajatendu Das. Advances in Active Radar Seeker Technology , 2005 .
[15] Xiao Du,et al. The study of guidance performance of a phased array seeker with platform , 2017 .
[16] Yu Yang,et al. Stability analysis of spinning missiles induced by seeker disturbance rejection rate parasitical loop , 2019 .
[17] Qunli Xia,et al. Beam-pointing error compensation method of phased array radar seeker with phantom-bit technology , 2017 .
[18] Yi Huang,et al. On extended state based Kalman filter design for a class of nonlinear time-varying uncertain systems , 2018, Science China Information Sciences.
[19] Bin Li,et al. Dynamic stability of rolling missiles with angle-of-attack feedback three-loop autopilot considering parasitic effect , 2017 .
[20] Naresh K. Sinha,et al. Modern Control Systems , 1981, IEEE Transactions on Systems, Man, and Cybernetics.
[21] Song Tian,et al. Dynamic stability of rolling missile with proportional navigation & PI autopilot considering parasitic radome loop , 2017 .
[22] Wei Wang,et al. The research of loop-shaping method to mitigate the total error effect in air-to-air missiles , 2019 .
[23] Warren W. Willman,et al. Effects of strapdown seeker scale-factor uncertainty on optimal guidance , 1988 .
[24] Paul Zarchan,et al. Tactical and strategic missile guidance , 1990 .