RELATIVE GPS NAVIGATION FOR H-II TRANSFER VEHICLE: DESIGN AND ON-ORBIT RESULTS

被引：0

作者：

Yoshikawa, Shoji ^{[1
]}

Suzuki, Masaharu ^{[2
]}

Tsukui, Jun ^{[3
]}

Yamamoto, Hifumi ^{[4
]}

Kasai, Toru ^{[5
]}

机构：

[1] Mitsubishi Electr Corp, Adv Technol R&D Ctr, Space Syst Grp, Tsukaguchi Honmachi 8-1-1, Amagasaki, Hyogo 6618661, Japan

[2] Mitsubishi Electr Corp, Kamakura Works, Kamakura, Kanagawa 2478520, Japan

[3] Mitsubishi Electr Corp, Kamakura Div, Space System Solut Dept, Kamakura, Kanagawa 2470065, Japan

[4] Mitsubishi Electr Corp, Tsukuba Div, Space Transportat Syst Grp, Space & Ground Systems Dept, Tsukuba, Ibaraki 3050032, Japan

[5] Japan Aerosp Explorat Agcy, HTV Project Team, Tsukuba, Ibaraki 3058505, Japan

来源：

SPACEFLIGHT MECHANICS 2011, PTS I-III | 2011年 / 140卷

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Relative GPS navigation (RGPS) filter estimates relative position and velocity of H-II Transfer Vehicle (HTV) based on GPS signals received by GPS receivers on HTV and International Space Station (ISS). It starts about several hundreds of thousand meters from ISS when proximity communication between HTV and ISS is established and hands over to the next navigation sensor (rendezvous sensor) at five hundred meters below the ISS. We will describe the design philosophy of the RGPS filter and report its performance results during the verification flight of HTV in September of 2009.

引用

页码：613 / +

页数：2