Deep-Space Optical Communication System (DOCS) for ESA's Space Weather Mission to Lagrange Orbit L5

被引:0
|
作者
Sodnik, Zoran [1 ]
Heese, Clemens [1 ]
Arapoglou, Pantelis-Daniel [1 ]
Schulz, Klaus-Juergen [2 ]
Zayer, Igor [2 ]
Daddato, Robert [2 ]
Kraft, Stefan [2 ]
机构
[1] European Space Agcy, European Space Res & Technol Ctr, Noordwijk, Netherlands
[2] European Space Agcy, European Space Operat Ctr, Darmstadt, Germany
来源
2017 IEEE INTERNATIONAL CONFERENCE ON SPACE OPTICAL SYSTEMS AND APPLICATIONS (ICSOS) | 2017年
关键词
DOCS; L5; Optel-mu; Optel-D; SSA; SWE; DST; DGT; deep-space optical communication; optical communication terminal; optical ground station;
D O I
暂无
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
ESA plans to embark the Deep-space Optical Communications System (DOCS) on the Space WEather (SWE) mission to the Sun-Earth Lagrange point L5 in the frame of its Space Situational Awareness (SSA) program. DOCS is an in orbit technology demonstration that also serves a scientific objective, namely the transfer of high-resolution solar imagery. The characteristics of the SWE L5 mission provide substantial advantages for deep-space optical communication, because the equidistant triangular orbital geometry between the sun, the Earth, and L5 (all three distances are equal to 1 AU approximate to 150 million kin) ensures that the sun is always separated by 60 degrees from both the space and the ground terminal. This allows for very efficient solar stray-light shielding and thermal management. It also reduces the pointing requirements of the DOCS Space Terminal (DST); a coarse pointing mechanism is not required, nor is a point-ahead assembly. The SSA SWE L5 mission Phase A, Phase B1 and B2 studies to be conducted 2017-2019 will take into account the accommodation and interfacing of the DST. DOCS aims to demonstrate a data rate of 10 Mbps over 1 AU to a 4-meter optical ground station. The development of the DST will follow a similar approach as foreseen for the Asteroid Impact Mission (AIM), namely to increase the technology readiness level (TRL) of existing developments wherever possible, or reasonable. The DST will be located on a side panel of the S/C, and will constantly face the Earth. Residual attitude movements (pointing errors) of the S/C will be covered by the field-of view of the DST telescope (an aperture diameter of 200 mm is envisaged) and by a fine pointing assembly. ESA is also embarking on a study to develop a 4-meter class DOCS ground terminal (DGT). Furthermore, the Consultative Committee for Space Data Systems (CCSDS) is currently developing a standard ("Blue Book") for "High Photon Efficiency Optical Communications". DOCS will serve as one of two implementations of the standard, which are required for it to become applicable.
引用
收藏
页码:28 / 33
页数:6
相关论文
共 50 条
  • [41] Optimization of an Optical Array Receiver for Deep-Space Optical Communication during Earth-Mars Conjunction Phase
    Hashmi, Ali Javed
    Eftikhar, Ali
    Adibi, Ali
    Amoozegar, Farid
    2012 PHOTONICS GLOBAL CONFERENCE (PGC), 2012,
  • [42] Space Weather Monitor at the L5 Point: A Case Study of a CME Observed with STEREO B
    Rodriguez, L.
    Scolini, C.
    Mierla, M.
    Zhukov, A. N.
    West, M. J.
    SPACE WEATHER-THE INTERNATIONAL JOURNAL OF RESEARCH AND APPLICATIONS, 2020, 18 (10):
  • [43] OPTEL-D - An Optical Communication System for the Deep Space
    Stumpf, Max
    Roth, Christoph
    Mosberger, Martin
    Francou, Laurent
    Reyes Garcia-Talavera, Marcos
    Heese, Clemens
    Sodnik, Zoran
    FREE-SPACE LASER COMMUNICATION AND ATMOSPHERIC PROPAGATION XXX, 2018, 10524
  • [44] A Kalman filter based synchronization scheme for telescope array receivers in deep-space optical communication links
    Hashmi, Ali Javed
    Eftekhar, Ali
    Adibi, Ali
    Amoozegar, Farid
    OPTICS COMMUNICATIONS, 2012, 285 (24) : 5037 - 5043
  • [45] Photon counting camera for the NASA deep space optical communication demonstration on the PSYCHE mission
    Buck, Benjamin R.
    Allen, Gregory D.
    Duerr, Erik K.
    McIntosh, K. Alexander
    Moynihan, Shawn T.
    Shukla, Vishwa N.
    Wang, Jeffrey D.
    ADVANCED PHOTON COUNTING TECHNIQUES XIII, 2019, 10978
  • [46] The deep-space multi-object orbit determination system and its application to Hayabusa2’s asteroid proximity operations
    Hiroshi Takeuchi
    Kent Yoshikawa
    Yuto Takei
    Yusuke Oki
    Shota Kikuchi
    Hitoshi Ikeda
    Stefania Soldini
    Naoko Ogawa
    Yuya Mimasu
    Go Ono
    Fuyuto Terui
    Naoya Sakatani
    Manabu Yamada
    Toru Kouyama
    Shingo Kameda
    Takanao Saiki
    Yuichi Tsuda
    Astrodynamics, 2020, 4 : 377 - 392
  • [47] The Vigil Magnetometer for Operational Space Weather Services From the Sun-Earth L5 Point
    Eastwood, J. P.
    Brown, P.
    Magnes, W.
    Carr, C. M.
    Agu, M.
    Baughen, R.
    Berghofer, G.
    Hodgkins, J.
    Jernej, I.
    Moestl, C.
    Oddy, T.
    Strickland, A.
    Vitkova, A.
    SPACE WEATHER-THE INTERNATIONAL JOURNAL OF RESEARCH AND APPLICATIONS, 2024, 22 (06):
  • [48] Performance Analysis of Free Space Optical Communication System for S, C and L band
    Jain, Deeksha
    Mehra, Rekha
    2017 INTERNATIONAL CONFERENCE ON COMPUTER, COMMUNICATIONS AND ELECTRONICS (COMPTELIX), 2017, : 183 - 189
  • [49] On-orbit space optical communication demonstration with a 22 s acquisition time
    Wang, Xuan
    Han, Junfeng
    Cui, Kai
    Wang, Chen
    Xie, Meilin
    Meng, Xiangsheng
    Chang, Zhiyuan
    OPTICS LETTERS, 2023, 48 (22) : 5980 - 5983
  • [50] The deep-space multi-object orbit determination system and its application to Hayabusa2's asteroid proximity operations
    Takeuchi, Hiroshi
    Yoshikawa, Kent
    Takei, Yuto
    Oki, Yusuke
    Kikuchi, Shota
    Ikeda, Hitoshi
    Soldini, Stefania
    Ogawa, Naoko
    Mimasu, Yuya
    Ono, Go
    Terui, Fuyuto
    Sakatani, Naoya
    Yamada, Manabu
    Kouyama, Toru
    Kameda, Shingo
    Saiki, Takanao
    Tsuda, Yuichi
    ASTRODYNAMICS, 2020, 4 (04) : 377 - 392