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近地卫星星历的高精度星载算法研究 被引量:7
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作者 张晓坤 刘迎春 +1 位作者 杨新 林宝军 《航天控制》 CSCD 北大核心 2005年第4期41-44,共4页
随着星载计算机系统结构和性能的改善,利用星载计算机实现高精度的星历计算成为可能。本文针对近地轨道卫星提出了一种适合星上轨道预报的数值算法。通过采用简化的动力学模型和一种嵌套插值算法的积分器,有效提高了计算效率,降低了对... 随着星载计算机系统结构和性能的改善,利用星载计算机实现高精度的星历计算成为可能。本文针对近地轨道卫星提出了一种适合星上轨道预报的数值算法。通过采用简化的动力学模型和一种嵌套插值算法的积分器,有效提高了计算效率,降低了对星载计算系统的性能要求,从而实现高精度的卫星星历星载计算。该算法在星载计算机系统平台上进行仿真验证的结果表明,对于某飞行器可实现轨道预报1天优于1km的星历计算。 展开更多
关键词 近地卫星 星历 轨道预报 数值积分 星载算法
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单点定位与实时定轨的星载算法的比较研究 被引量:2
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作者 刘峰 巨涛 《飞行器测控学报》 2007年第4期25-29,共5页
卫星单点定位方法和卫星定轨方法均采用GPS接收机测量得到的伪距和伪距率作为原始观测量。前者依据几何学原理,采用最小二乘法对单个历元的原始观测量进行处理,解算出卫星的位置和速度;而后者依据轨道动力学理论,采用卡尔曼滤波方... 卫星单点定位方法和卫星定轨方法均采用GPS接收机测量得到的伪距和伪距率作为原始观测量。前者依据几何学原理,采用最小二乘法对单个历元的原始观测量进行处理,解算出卫星的位置和速度;而后者依据轨道动力学理论,采用卡尔曼滤波方法通过连续的原始观测量对滤波器状态量的修正使定轨结果收敛。通过比较,星载定轨方法能够明显改善定位测速的精度和数据的稳定性,其外推功能可以有效避免观测量短时间中断对定轨结果连续性的影响。我们已经将实时定轨算法应用到星载型号任务的工程中,并取得了较好的结果。 展开更多
关键词 星载算法 定位 定轨
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OPTIMIZATION ON ANTENNA PATTERN OF SPACEBORNE SAR WITH IMPROVED NSGA-Ⅱ 被引量:2
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作者 Xiao Jiang Wang Xiaoqing +1 位作者 Zhu Minhui Xiao Liu 《Journal of Electronics(China)》 2009年第4期443-447,共5页
Optimization of antenna array pattern used in a spaceborne Synthetic Aperture Radar (SAR) system is considered in this study. A robust evolutionary algorithm, Non-dominated Sorting Genetic Algorithms (the improved NS... Optimization of antenna array pattern used in a spaceborne Synthetic Aperture Radar (SAR) system is considered in this study. A robust evolutionary algorithm, Non-dominated Sorting Genetic Algorithms (the improved NSGA-Ⅱ), is applied on a spaceborne SAR antenna pattern design. The system consists of two objective functions with two constraints. Pareto fronts are generated as a result of multi-objective optimization. After being validated by a test problem ZDT4, the algorithms are used to synthesize spaceborne SAR antenna radiation pattern. The good results with low Ambi- guity-to-Signal Ratio (ASR) and high directivity are obtained in the paper. 展开更多
关键词 Synthetic Aperture Radar (SAR) Radiation pattern Improved Non-dominated Sorting Genetic Algorithms (NSGA)-Ⅱ Ambiguity-to-Signal Ratio (ASR)
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Multipath error detection and correction for GEO/IGSO satellites 被引量:33
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作者 WU XiaoLi ZHOU JianHua +2 位作者 WANG Gang HU XiaoGong CAO YueLing 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2012年第7期1297-1306,共10页
Constellations of regional satellite navigation systems are usually constituted of geostationary satellites (GEO) and inclined geostationary satellites (IGSO) for better service availability. Analysis of real data sho... Constellations of regional satellite navigation systems are usually constituted of geostationary satellites (GEO) and inclined geostationary satellites (IGSO) for better service availability. Analysis of real data shows that the pseudorange measurements of these two types of satellites contain significant multipath errors and code noise, and the multipath for GEO is extremely serious, which is harmful to system services. In contrast, multipath error of carrier phase measurements is less than 3 cm, which is smaller than the multipath of pseudorange measurements by two orders of magnitude. Using a particular combination of pseudorange and dual-frequency carrier phase measurements, the pseudorange multipath errors are detected, and their time varying features are analyzed. A real-time multipath correction algorithm is proposed in this paper, which is called CNMC (Code Noise and Multipath Correction). The algorithm decreases the influence of the multipath error and therefore ensures the performance of the system. Data processing experiments show that the multipath error level may be reduced from 0.5 m to 0.15 m by using this algorithm, and 60% of GEO multipath errors and 42% of IGSO multipath errors are successfully corrected with CNMC. Positioning experiments are performed with a constellation of 3 GEO plus 3 IGSO satellites. For dual-frequency users the East-West position accuracy is improved from 1.31 m to 0.94 m by using the CNMC algorithm, the South-North position accuracy is improved from 2.62 m to 2.29 m, and the vertical position accuracy is improved from 4.25 m to 3.05 m. After correcting multipath errors, the three-dimensional position accuracy is improved from 5.16 m to 3.94 m. 展开更多
关键词 multipath error carrier smoothing pseudorange GEO satellite position error
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