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挠性捷联惯组的多位置对准技术 被引量:4
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作者 芦佳振 张春熹 魏莹莹 《系统工程与电子技术》 EI CSCD 北大核心 2012年第3期562-567,共6页
弹用惯组的误差是影响系统落点导航精度的关键因素。针对如何利用已知的航向信息最大程度地提高弹用挠性陀螺的实际使用精度的问题,将多位置对准技术应用于惯组误差的在线标定,利用行列式法对陀螺静态漂移误差进行了可观性分析,给出常... 弹用惯组的误差是影响系统落点导航精度的关键因素。针对如何利用已知的航向信息最大程度地提高弹用挠性陀螺的实际使用精度的问题,将多位置对准技术应用于惯组误差的在线标定,利用行列式法对陀螺静态漂移误差进行了可观性分析,给出常用两位置对准的理论分析及最优三位置的限定方程。仿真结果表明,最优三位置对准可以有效分离常值漂移和与比力一次项有关的漂移,实现挠性陀螺静态漂移误差状态变量全部可观测,最大程度地降低其对系统误差的影响。 展开更多
关键词 挠性捷联惯组 多位置对准 标定 误差模型 比力敏感误差
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Control failure of the roll-isolated inertial navigation system under large pitch angle 被引量:3
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作者 Jinchao SONG Shuxing YANG Fenfen XIONG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2020年第10期2707-2715,共9页
Roll-isolation is an effective way for spinning vehicle to greatly reduce the roll gyro range of strapdown Inertial Navigation System(SINS)and increase the accuracy of inertial navigation.However,during a recent fligh... Roll-isolation is an effective way for spinning vehicle to greatly reduce the roll gyro range of strapdown Inertial Navigation System(SINS)and increase the accuracy of inertial navigation.However,during a recent flight test,the roll-isolated control system failure was observed under a large pitch angle(706 h 685),which introduces a sharply increase in the roll angular velocity,the saturation of roll gyro and the inertial navigation failure.To address this issue,the governing equation of the roll-isolated system is derived with the consideration of various disturbance factors.The control failure is reproduced by numerical simulation.And the results show that the pitch and yaw angular velocity can cause a dramatic increase in roll rate under the large pitch angle,resulting in the roll-isolated control failure.Meanwhile,an improved roll-isolated control system is developed using PI controller,which is verified by mathematical simulation. 展开更多
关键词 Spinning vehicle strap-down inertial navigation system(sins) Roll-isolated control Control failure Large pitch angle
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无迹卡尔曼滤波和无迹粒子滤波在惯导初始对准中的应用对比 被引量:5
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作者 蒋治宇 郭承军 《科学技术与工程》 北大核心 2018年第7期267-270,共4页
捷联惯性导航系统是新型航位推算系统,在惯导系统执行工作任务之前需要进行初始对准,以保证系统的正常运行。对捷联式惯导系统,初始对准就是确定初始时刻的姿态阵,利用惯性元件的输出信息,选用合适的滤波方法,将计算的导航坐标系与真实... 捷联惯性导航系统是新型航位推算系统,在惯导系统执行工作任务之前需要进行初始对准,以保证系统的正常运行。对捷联式惯导系统,初始对准就是确定初始时刻的姿态阵,利用惯性元件的输出信息,选用合适的滤波方法,将计算的导航坐标系与真实导航坐标系的失准角估计出来,来修正姿态矩阵,使计算坐标系与真实坐标系尽可能重合。在实际的导航系统中,状态方程和量测方程通常都是非线性的,对于非线性特性,传统的解决方法是利用EKF滤波算法,但它只适用于弱非线性模型的估计,系统的非线性越强,引起的估计误差就越大,甚至会引起滤波发散。为此提出两种滤波算法无迹卡尔曼滤波UKF与无迹粒子滤波UPF,并将两者进行了仿真对比,结果表明(UPF)算法比(UKF)算法收敛速度更快,估计精度更高。 展开更多
关键词 捷联惯导(sins) 初始对准 滤波 无迹卡尔曼滤波(UKF) 无迹粒子滤波(UPF)
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Adaptive Dual Wavelet Threshold Denoising Function Combined with Allan Variance for Tuning FOG-SINS Filter 被引量:1
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作者 BESSAAD Nassim BAO Qilian +3 位作者 SUN Shuodong DU Yuding LIU Lin HASSAN Mahmood Ul 《Journal of Shanghai Jiaotong university(Science)》 EI 2020年第4期434-440,共7页
Allan variance(AV)stochastic process identification method for inertial sensors has successfully combined the wavelet transform denoising scheme.However,the latter usually employs a traditional hard threshold or soft ... Allan variance(AV)stochastic process identification method for inertial sensors has successfully combined the wavelet transform denoising scheme.However,the latter usually employs a traditional hard threshold or soft threshold that presents some mathematical problems.An adaptive dual threshold for discrete wavelet transform(DWT)denoising function overcomes the disadvantages of traditional approaches.Assume that two thresholds for noise and signal and special fuzzy evaluation function for the signal with range between the two thresholds assure continuity and overcome previous difficulties.On the basis of AV,an application for strap-down inertial navigation system(SINS)stochastic model extraction assures more efficient tuning of the augmented 21-state improved exact modeling Kalman filter(IEMKF)states.The experimental results show that the proposed algorithm is superior in denoising performance.Furthermore,the improved filter estimation of navigation solution is better than that of conventional Kalman filter(CKF). 展开更多
关键词 Allan variance(AV) discrete wavelet transform(DWT) adaptive dual threshold fiber optic gyroscope(FOG) strap-down inertial navigation system(sins) exact modeling filter
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