共查询到19条相似文献,搜索用时 140 毫秒
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用四无数法设计一种新型动基座初始对准 总被引:1,自引:1,他引:0
利用捷联制导系统固有的硬件资源可构造一种新型的动基座初始对准方案,运用广义卡尔曼滤波技术及四元数法表示,给出了实施初始对准的失调估计器的设计方法,仿真结果表明,该设计可有效地在飞行过程中实施快速初始对准。 相似文献
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对于要求快速反应能力的导弹武器系统,初始对准难以满足武器系统对快速性的要求.这种情况下,发射平台只提供简单的初始化,对准过程在导弹飞行过程中完成,这种方法称为飞行中对准.建立了飞行中对准的数学模型,通过仿真计算研究飞行中对准的性能以及影响对准性能的因素. 相似文献
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舰载捷联惯导动基座 F-QUEST 初始对准方法 总被引:2,自引:0,他引:2
针对目前基于惯性系的捷联惯导动基座对准方法信息利用率不高及矢量观测选取不确定性导致对准精度下降的问题,提出了一种新的舰载捷联惯导动基座滤波四元数估计(filter quaternion estimation,F-QUEST)对准方法。构建了捷联惯导动基座初始对准模型,并利用姿态矩阵链式法则将惯导初始对准转化为姿态确定问题,进而采用 F-QUEST 算法求取姿态矩阵以实现捷联惯导动基座对准。车载试验结果表明:相比传统方法,新方法具有更高的对准精度和更快的收敛速度,水平姿态角误差只需3 s 即可收敛到0.01°。 相似文献
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采用直接装订的方法来完成捷联惯导系统的初始对准,虽然可以提高战术导弹的快速反应性,但是也引入了初始对准误差.该误差虽然较小,但造成导弹命中精度的影响不可忽略.为了补偿这种影响,研究了一种借助地面雷达站提供导弹的导航信息,把初始对准误差给分离出来的方法. 相似文献
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Nonlinear initial alignment is a significant research topic for strapdown inertial navigation system(SINS).Cubature Kalman filter(CKF)is a popular tool for nonlinear initial alignment.Standard CKF assumes that the statics of the observation noise are pre-given before the filtering process.Therefore,any unpredicted outliers in observation noise will decrease the stability of the filter.In view of this problem,improved CKF method with robustness is proposed.Multiple fading factors are introduced to rescale the obser-vation noise covariance.Then the update stage of the filter can be autonomously tuned,and if there are outliers exist in the observations,the update should be less weighted.Under the Gaussian assumption of KF,the Mahalanobis distance of the innovation vector is supposed to be Chi-square distributed.Therefore a judging index based on Chi-square test is designed to detect the noise outliers,determining whether the fading tune are required.The proposed method is applied in the nonlinear alignment of SINS,and vehicle experiment proves the effective of the proposed method. 相似文献
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《防务技术》2010,(2)
To know the temperature status of track and wheels on tank,the finite element calculation of temperature field was implemented with ANSYS software.The detailed temperature distributions for road wheel,drive wheel,idle wheel and track loop were obtained.The effect of factors,such as tank speed,environment temperature,sun radiant energy,ground deformation resistant and tank load,on the temperature of road wheel was studied.The sensitivity analysis shows that the effect of tank load on the temperature is the most,and the effect of ground deformation resistant is the least.The temperature testing device for road wheel on tank was developed to perform the experiments in real time.The calculated temperatures are in accord well with the experimental values. 相似文献
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在SINS(捷联式惯性导航系统)与GPS(全球定位系统)组合传递对准时,航向角的可观测性较弱,经过卡尔曼滤波后,航向角误差虽有所改善,但仍呈发散趋势,针对GPS/SINS组合系统特点,提出了一种动基座传递对准方案,依靠GPS测量信息进行速度匹配,完成动基座传递对准.该方案采用粒子滤波方法解决对准过程中的非线性问题.仿真结果表明该方案的对准精度(1σ)可以达到东向失准角误差为5角分,北向失准角误差为2角分,方位失准角误差为6角分. 相似文献
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《防务技术》2020,16(1):257-262
The rapidity and accuracy of the initial alignment influence the performance of the strapdown inertial navigation system (SINS), compass alignment is one of the most important methods for initial alignment. The selection of the parameters of the compass alignment loop directly affects the result of alignment. Nevertheless, the optimal parameters of the compass loop of different SINS are also different. Traditionally, the alignment parameters are determined by experience and trial-and-error, thus it cannot ensure that the parameters are optimal. In this paper, the Genetic Algorithm-Particle Swarm Optimization (GA-PSO) algorithm is proposed to optimize the compass alignment parameters so as to improve the performance of the initial alignment of strapdown gyrocompass. The experiment results showed that the GA-PSO algorithm can find out the optimal parameters of the compass alignment circuit quickly and accurately and proved the effectiveness of the proposed method. 相似文献
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潜艇自航式诱饵组合使用方法的优劣主要评判依据是使用的方法最终使得潜艇对抗鱼雷成功的概率,对抗时间和诱骗距离是影响对抗成功概率的两个重要因素,它们又主要围绕发射时机、初始航向以及潜艇机动等几个问题展开。该文通过分析各个诱饵的作战使命,在一定态势下,根据诱饵的性能、鱼雷报警距离及舷角等各方面因素,建立大小口径声诱饵协同作战的弹道模型,并由此得到了诱饵发射时机、初始航向等参数。 相似文献
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固定基座发射的弹道式导弹,可以利用三轴陀螺平台罗盘系统来实现全方位自对准。在考虑到系统噪声及测量噪声情况下,根据离散型线性随机系统最优控制的分离定理,实现平台罗盘自对准系统的最优控制。计算结果表明,所讨论的方法,可以在对准精度、对准时闻及对随机干扰信号的滤波作用诸性能要求方面,获得满意的结果。 相似文献