发明名称 SATELLITE OBSERVATION PLAN PROGRAM AND SATELLITE OBSERVATION PLANNING DEVICE
摘要 PROBLEM TO BE SOLVED: To specify a satellite which is used for observing an observational target position most quickly, out of a plurality of satellites. SOLUTION: In a satellite observation plan program, when an observation condition is inputted, an absolute valueΔR of a difference between a satellite position vector and an observational target position vector at a time T (S16 in the figure), and it is determined whether theΔR is less than the maximum slant rangeρmax or not (S17). When theΔR is less than theρmax, the time T is stored in a memory as an observable time (S21). The above process is performed for each of a plurality of satellites to specify a satellite which is used for observing the observational target position most quickly. COPYRIGHT: (C)2008,JPO&INPIT
申请公布号 JP2008081049(A) 申请公布日期 2008.04.10
申请号 JP20060265946 申请日期 2006.09.28
申请人 FUJITSU LTD 发明人 AOKI HIROKO
分类号 B64G3/00;G01W1/08 主分类号 B64G3/00
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