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
  • [21] Structural dynamic responses of a stripped solar sail subjected to solar radiation pressure
    Zhang, Junhui
    Wu, Na
    Tong, An
    Liu, Yinghua
    CHINESE JOURNAL OF AERONAUTICS, 2020, 33 (08) : 2204 - 2211
  • [22] A curved surface solar radiation pressure force model for solar sail deformation
    He Jing
    Gong ShengPing
    Li JunFeng
    SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2012, 55 (01) : 141 - 155
  • [23] HYBRID SWITCHING ATTITUDE CONTROL OF UNDERACTUATED SPACECRAFT SUBJECT TO SOLAR RADIATION PRESSURE
    Petersen, Chris
    Leve, Frederick
    Kolmanovsky, Ilya
    SPACEFLIGHT MECHANICS 2015, PTS I-III, 2015, 155 : 3225 - 3243
  • [24] Symmetries in the optimal control of solar sail spacecraft
    Kim, M
    Hall, CD
    CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2005, 92 (04): : 273 - 293
  • [25] FLIGHT PATH CONTROL FOR SOLAR SAIL SPACECRAFT
    Wawrzyniak, Geoffrey G.
    Howell, Kathleen C.
    SPACEFLIGHT MECHANICS 2012, 2012, 143 : 1349 - +
  • [26] Symmetries in the Optimal Control of Solar Sail Spacecraft
    M. Kim
    C. D. Hall
    Celestial Mechanics and Dynamical Astronomy, 2005, 92 : 273 - 293
  • [27] An attitude control strategy for spinning solar sail
    Institute of Space and Astronautical Science, JAXA, Japan
    IFAC Proc. Vol. (IFAC-PapersOnline), PART 1 (401-406):
  • [28] OPTIMAL-CONTROL OF A SPACECRAFT WITH A SOLAR SAIL
    GULYAEV, VI
    KOSHKIN, VL
    VASILEV, AB
    INTERNATIONAL APPLIED MECHANICS, 1994, 30 (09) : 721 - 726
  • [29] An experiment on dynamical analysis of spinning solar sail
    Okui, T
    SPACE ACTIVITIES AND COOPERATION CONTRIBUTING TO ALL PACIFIC BASIN COUNTRIES, 2004, 117 : 63 - 70
  • [30] Attitude Control of Solar Sail Spacecraft with Saturation
    Wei Yiheng
    Zhu Min
    Peng Cheng
    Wang Yong
    PROCEEDINGS OF THE 31ST CHINESE CONTROL CONFERENCE, 2012, : 2668 - 2672