Space high-accuracy intelligence payload system with integrated attitude and position determination

被引:5
|
作者
LI Jin [1 ,2 ,3 ]
XING Fei [1 ,2 ,3 ]
SUN Ting [1 ,2 ,3 ]
LIU Zengyi [1 ,2 ,3 ]
YOU Zheng [1 ,2 ,3 ]
机构
[1] Department of precision instrument,Tsinghua University
[2] State Key Laboratory of Precision Measurement Technology and Instruments  3. Collaborative Innovation Center for Micro / Nano Fabrication,Device and System
基金
国家高技术研究发展计划(863计划);
关键词
earth observation; intelligence payload; optical remote sensors;
D O I
10.15878/j.cnki.instrumentation.2015.01.002
中图分类号
V443.5 [];
学科分类号
08 ; 0825 ;
摘要
recently,the requirements for space high resolution and high accuracy earth observation payloads are more urgent in many fields.However,traditional satellites mainly use the separation model of platform and payload.The precision of platform was unable to fulfill the requirements of high-precision imaging of payload.In addition,because traditional satellites mainly use the rigid connection between platform and payload,the precision of payload strongly depends on platform.They make satellite development and requirements increasingly difficult.To solve these disadvantages,in this paper,we introduce a Space High-accuracy integrated Intelligence Payload(SHIP) system with real-time attitude and position determination.SHIP can complete real time autonomous high accuracy attitude and position determination,high resolution remote sensing imaging,high-accuracy target position based on image,multi-mode motion imaging and target identification,tracking,self-recovery function of on orbit image,self-determination function of attitude and position,and so on.
引用
收藏
页码:3 / 16
页数:14
相关论文
共 50 条
  • [1] High-Accuracy Self-Calibration for Smart, Optical Orbiting Payloads Integrated with Attitude and Position Determination
    Li, Jin
    Xing, Fei
    Chu, Daping
    Liu, Zilong
    SENSORS, 2016, 16 (08)
  • [2] Experiment on GPS based high-accuracy attitude determination
    Wang, Y.H.
    Hu, X.P.
    Yuhang Xuebao/Journal of Astronautics, 2001, 22 (01):
  • [3] High-accuracy measuring system for position and attitude in pushing-bridge construction based on machine vision
    School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2007, 33 (03): : 322 - 326
  • [4] A MEMS-BASED MULTI-SENSOR SYSTEM FOR SATELLITE HIGH-ACCURACY ATTITUDE DETERMINATION
    Merkuryev, Igor V.
    FIRST IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2012, PTS I AND II, 2012, 145 : 365 - 378
  • [5] Integrity monitoring of high-accuracy GNSS-based attitude determination
    Na Li
    Lin Zhao
    Liang Li
    Chun Jia
    GPS Solutions, 2018, 22
  • [6] HIGH-ACCURACY ATTITUDE DETERMINATION FOR THE X-RAY-SATELLITE ROSAT
    RUPP, T
    SCHNEIDERS, G
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (03) : 554 - 561
  • [7] Integrity monitoring of high-accuracy GNSS-based attitude determination
    Li, Na
    Zhao, Lin
    Li, Liang
    Jia, Chun
    GPS SOLUTIONS, 2018, 22 (04)
  • [8] Constrained Wrapped Least Squares: A Tool for High-Accuracy GNSS Attitude Determination
    Liu, Xing
    Ballal, Tarig
    Chen, Hui
    Al-Naffouri, Tareq Y.
    IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2022, 71
  • [9] High-accuracy attitude angle measurement system using laser collimation
    Pan, Ning
    Zhao, Qin
    Wu, Yanpeng
    Yuan, Li
    Bai, Jian
    APPLIED OPTICS, 2024, 63 (19) : F67 - F73
  • [10] High-Accuracy Heading Determination
    El-Osery, Aly
    Bruder, Stephen
    Laughlin, Darren
    2013 8TH INTERNATIONAL CONFERENCE ON SYSTEM OF SYSTEMS ENGINEERING (SOSE), 2013, : 308 - 313