GPSを利用した月軌道宇宙機の測位について On Navigation of Lunar Orbiter by Utilizing GPS

この論文にアクセスする

この論文をさがす

著者

抄録

The purpose of this paper is to discuss the method and accuracy of position determination of a spacecraft at a long distance from the earth like a lunar orbiter. Several very long base-lines which start at a main radio station, spread out in any directions and end at several subordinate radio stations are used to measure differences in the time of arrival of the radio signal transmitted from the spacecraft. Precise measurements of positions and clock offsets of subordinate stations relative to the main station are required to achieve the accurate position determination. The method and the accuracy of the position and clock offset determination of radio stations by using GPS satellites as radio sources of the interferometry measurements are investigated and the following accuracy of the space navigation is shown by simple equations.

収録刊行物

  • 日本航空宇宙学会誌 = Journal of the Japan Society for Aeronautical and Space Sciences  

    日本航空宇宙学会誌 = Journal of the Japan Society for Aeronautical and Space Sciences 45(516), 18-28, 1997-01 

    一般社団法人 日本航空宇宙学会

参考文献:  11件

参考文献を見るにはログインが必要です。ユーザIDをお持ちでない方は新規登録してください。

各種コード

  • NII論文ID(NAID)
    10002861268
  • NII書誌ID(NCID)
    AN00189072
  • 本文言語コード
    JPN
  • 資料種別
    ART
  • ISSN
    00214663
  • NDL 記事登録ID
    4117315
  • NDL 雑誌分類
    ZN25(科学技術--運輸工学--航空機・ロケット)
  • NDL 請求記号
    Z16-436
  • データ提供元
    CJP書誌  NDL  J-STAGE 
ページトップへ