JP6027824B2 - 衛星測位のための軌道パラメータ生成方法、生成プログラム、並びに、衛星測位システム - Google Patents
衛星測位のための軌道パラメータ生成方法、生成プログラム、並びに、衛星測位システム Download PDFInfo
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- JP6027824B2 JP6027824B2 JP2012197473A JP2012197473A JP6027824B2 JP 6027824 B2 JP6027824 B2 JP 6027824B2 JP 2012197473 A JP2012197473 A JP 2012197473A JP 2012197473 A JP2012197473 A JP 2012197473A JP 6027824 B2 JP6027824 B2 JP 6027824B2
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| JP2012197473A JP6027824B2 (ja) | 2012-09-07 | 2012-09-07 | 衛星測位のための軌道パラメータ生成方法、生成プログラム、並びに、衛星測位システム |
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| JP2014052306A JP2014052306A (ja) | 2014-03-20 |
| JP2014052306A5 JP2014052306A5 (enExample) | 2015-10-29 |
| JP6027824B2 true JP6027824B2 (ja) | 2016-11-16 |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US10795028B2 (en) * | 2016-12-20 | 2020-10-06 | Here Global B.V. | Supporting an extension of a validity period of parameter values defining an orbit |
| CN113901636B (zh) * | 2021-08-20 | 2025-09-26 | 航天科工火箭技术有限公司 | 火箭轨道参数的计算方法、终端设备及介质 |
| CN114826337A (zh) * | 2022-03-23 | 2022-07-29 | 中国科学院计算技术研究所 | 一种用于卫星通信信号的多普勒频偏的预补偿方法及系统 |
| CN115167498B (zh) * | 2022-08-23 | 2024-05-03 | 中国电子科技集团公司第三十八研究所 | 偏航导引低轨雷达成像卫星工作参数更新方法及系统 |
| CN116305923A (zh) * | 2023-03-16 | 2023-06-23 | 南京大学 | 一种应用于b/s架构下太阳系仿真的时空系统设计方法 |
| CN119881972B (zh) * | 2025-03-27 | 2025-05-27 | 中电科航空电子有限公司 | 卫星导航接收机观测数据及故障模拟注入方法、装置、设备及介质 |
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| JP3042456B2 (ja) * | 1997-08-18 | 2000-05-15 | 日本電気株式会社 | 測位衛星を用いた測位システム |
| US8493267B2 (en) * | 2006-11-10 | 2013-07-23 | Qualcomm Incorporated | Method and apparatus for position determination with extended SPS orbit information |
| US8514128B2 (en) * | 2010-09-02 | 2013-08-20 | eRide,. Inc. | Satellite navigation receivers with self-provided future ephemeris and clock predictions |
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