Hybrid Estimation of Solar Radiation Pressure for a Spinning Solar Sail Spacecraft

被引:7
|
作者
Yamaguchi, Tomohiro [1 ]
Mimasu, Yuya [2 ]
Tsuda, Yuichi [2 ]
Yoshikawa, Makoto [2 ]
机构
[1] GMV ESA ESOC, Mission Anal Sect, D-64293 Darmstadt, Germany
[2] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Chuo Ku, Sagamihara, Kanagawa 2525210, Japan
关键词
OPTICAL DEGRADATION; DEMONSTRATOR; MODEL;
D O I
10.2514/1.A32387
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A hybrid estimation technique was applied to determine the solar radiation pressure (SRP) force acting on the solar sail spacecraft Interplanetary Kite-craft Accelerated by Radiation of the Sun (IKAROS). To evaluate the SRP force, only tracking data obtained during coast arcs are used. The orbit determination and SRP parameters estimation is implemented using batch weighted least squares. The observables are X/X band two-way Doppler and range measurements. The actually encountered solar radiation pressure acceleration of the IKAROS spacecraft is found to amount to only 88% of the value of the prelaunch simulations. Furthermore, the hybrid technique improves the accuracy of the solar radiation pressure acceleration estimation almost by a factor of five. These results underline the importance of applying a hybrid evaluation of not only the solar radiation pressure force but also the torque for navigation of a solar sail spacecraft.
引用
下载
收藏
页码:381 / 384
页数:4
相关论文
共 50 条
  • [41] ATTITUDE AND ORBITAL MODELING OF SOLAR-SAIL SPACECRAFT
    ANGRILLI, F
    BORTOLAMI, S
    ESA JOURNAL-EUROPEAN SPACE AGENCY, 1990, 14 (04): : 431 - 446
  • [43] An integrated simulation system for operating solar sail spacecraft
    Zheng Yaru
    Li Qinglong
    Xu Ming
    Dong Yunfeng
    JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2021, 32 (05) : 1200 - 1211
  • [44] Control of the Spacecraft with a Solar Sail, Performing an Interplanetary Flight
    Gorbunova, Irina
    Starinova, Olga
    2015 7TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST), 2015, : 111 - 115
  • [45] On attainability of small bodies by use of the solar sail spacecraft
    Pomazanov, MV
    Yegorov, VA
    EXPLORATION OF SMALL BODIES IN THE SOLAR SYSTEM: I. INITIAL RESULTS AND FUTURE PROSPECTS, 1999, 24 (09): : 1175 - 1183
  • [46] FEEDBACK CONTROL OF THE SPACECRAFT WITH A SOLAR SAIL FOR INTERPLANETARY FLIGHTS
    Gorbunova, Irina
    Starinova, Olga
    THIRD IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2017, 2017, 161 : 315 - 324
  • [47] Optimal Attitude Maneuver of an Axisymmetric Spinning Solar Sail
    Gong, Shengping
    Li, Junfeng
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2015, 51 (02) : 1462 - 1474
  • [48] Flexibility influence on passive stability of a spinning solar sail
    Hu, Xiaosai
    Gong, Shengping
    AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 58 : 60 - 70
  • [49] Attitude control of spinning solar sail with huge membrane
    Hanaoka, Fuminori
    Mori, Osamu
    Tsuda, Yuichi
    Funase, Ryu
    Kawaguchi, Jun'ichiro
    SPACEFLIGHT MECHANICS 2008, VOL 130, PTS 1 AND 2, 2008, 130 : 1765 - +
  • [50] Self-excited oscillation of spinning solar sails utilizing solar radiation pressure
    Takao, Yuki
    Mori, Osamu
    Kawaguchi, Jun'ichiro
    ASTRODYNAMICS, 2020, 4 (03) : 177 - 192