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基于校准导航的广域电力系统负荷模型校准 被引量:2
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作者 郝丽丽 岳浩永 王昊昊 《电力自动化设备》 EI CSCD 北大核心 2016年第7期74-81,89,共9页
基于系统主导模式下功角稳定裕度关于各节点负荷参数的灵敏度分析,提出广域电力系统负荷模型的校准导航,以区分系统负荷模型的主导校准区域和主导校准参数,并分析节点的稳定群属特征。基于静态、动态负荷比例参数和负荷功率初值,讨论电... 基于系统主导模式下功角稳定裕度关于各节点负荷参数的灵敏度分析,提出广域电力系统负荷模型的校准导航,以区分系统负荷模型的主导校准区域和主导校准参数,并分析节点的稳定群属特征。基于静态、动态负荷比例参数和负荷功率初值,讨论电力系统负荷模型主导校准区域的分布规律及其影响因素,结果表明该类参数的主导校准区域分布主要取决于扰动的位置和各节点负荷有功功率的大小,仿真和实际算例验证了其正确性。提出先选择主导校准区域,再对其中负荷节点进行分类,并对同类负荷节点采用相同的模型参数进行统一校准的方案,以提高广域电力系统负荷模型校准的效率和精度。 展开更多
关键词 校准导航 广域电力系统 负荷模型 主导校准区域 主导校准参数 负荷分类
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基于单信标FDOA法的UUV长航程导航校准方法
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作者 宫榕杉 《声学与电子工程》 2022年第2期22-25,共4页
水下单信标导航系统具有系统复杂度低、灵活配置及隐蔽性高等特点,信标航路接近设计是UUV单信标自身惯导校准及成功定位的关键。文章首先对单信标基于频差(Frequency Difference Of Arrival,FDOA)导航原理进行介绍并对导航误差进行分析... 水下单信标导航系统具有系统复杂度低、灵活配置及隐蔽性高等特点,信标航路接近设计是UUV单信标自身惯导校准及成功定位的关键。文章首先对单信标基于频差(Frequency Difference Of Arrival,FDOA)导航原理进行介绍并对导航误差进行分析,然后依据导航误差分布规律优化设计了单信标导航信标接近路径,提出了长航程UUV导航校准流程。在设计的长航程仿真场景中,利用若干单信标,实现了UUV的惯导误差校准。 展开更多
关键词 无人水下航行器 单信标导航 频差导航 导航校准 接近航路设计
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Application of H_∞ filtering in the initial alignment of strapdown inertial navigation system 被引量:1
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作者 YUFei SUNFeng 《Journal of Marine Science and Application》 2005年第1期50-53,共4页
In this paper , the principle of H∞ filtering is discussed and H_∞ filter is constructed, which is used in the initial alignment of the strapdown inertial navigation systems(SINS). The error model of SINS is derived... In this paper , the principle of H∞ filtering is discussed and H_∞ filter is constructed, which is used in the initial alignment of the strapdown inertial navigation systems(SINS). The error model of SINS is derived. By utilizing constructed H∞ filter, the filtering calculation to that system has been conducted. The simulation results of the misalignment angle are given under the condition of unknown noises. The results show that the process of alignment with H∞ filter is much faster and with excellent robustness. 展开更多
关键词 H_∞ filtering initial alignment inertial navigation
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New self-calibration schemes for accelerometers in platform INS
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作者 Hong Cai Anliang Li Yuan Cao 《Journal of Systems Science & Complexity》 SCIE EI CSCD 2015年第5期1032-1042,共11页
To ensure success of precise navigation, it is necessary to carry out in-field calibration for the accelerometers in platform inertial navigation system(PINS) before a mission is launched.Traditional continuous self-c... To ensure success of precise navigation, it is necessary to carry out in-field calibration for the accelerometers in platform inertial navigation system(PINS) before a mission is launched.Traditional continuous self-calibration methods are not fit for fast calibration of accelerometers because the platform misalignments have to be estimated precisely and the nonlinear coupling terms will affect accuracy. The multi-position methods with a "shape of motion" algorithm also have some existing disadvantages: High precision calibration results cannot be obtained when the accelerometer's output data are used directly and it is difficult to optimize the calibration scheme. Focusing on this field, this paper proposes new fast self-calibration methods for the accelerometers of PINS. A data compression filter is employed to improve the accuracy of parameter estimation because it is impossible to obtain non-biased estimation for accelerometer parameters when using the "shape of motion" algorithm. Besides, continuous calibration schemes are designed and optimized by the genetic algorithm(GA) to improve the observability of parameters. Simulations prove that the proposed methods can estimate the accelerometer parameter more precisely than traditional continuous methods and multi-position methods, and they are more practical to deal with urgent situations than multi-position methods. 展开更多
关键词 SELF-CALIBRATION accelerometers data compression genetic algorithm
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