发明名称 Satellite orbit data compressing method, satellite orbit data providing method, satellite orbit data decompressing method, and data compressing device
摘要 A satellite orbit data compressing method includes: determining a compression method of a parameter value on the basis of a variation tendency of the parameter value in an orbit model approximating a satellite orbit; and calculating a compressed parameter value by reducing a bit sequence representing the parameter value using the determined compression method.
申请公布号 US8819289(B2) 申请公布日期 2014.08.26
申请号 US200912631969 申请日期 2009.12.07
申请人 Seiko Epson Corporation 发明人 Onda Kenji
分类号 G06F15/16;G01S19/05;G01S19/27;G01S19/25 主分类号 G06F15/16
代理机构 Global IP Counselors, LLP 代理人 Global IP Counselors, LLP
主权项 1. A satellite orbit data compression method comprising: determining a first compression method of a first set of values for a parameter in a first time period based on a first variation tendency of the first set of values in the first time period; compressing the first set of values using the first compression method; determining a second compression method of a second set of values for the parameter in a second time period based on a second variation tendency of the second set of values in the second time period, the second time period being longer than the first time period, the second variation tendency being different from the first variation tendency; and compressing the second set of values using the second compression method.
地址 Tokyo JP