A method of stellar-inertial attitude determination under high dynamic condition

被引：0
|
作者：
机构：
[1] Han, Li
[2] Zhang, Lijun
[3] Cai, Hong
[4] Zhang, Shifeng
来源：
Han, Li (hanli08@163.com) | 1767年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 40期
关键词：
Gyroscopes - Signal to noise ratio - Image enhancement - Stars - Kalman filters - Parameter estimation;
D O I：
10.13700/j.bh.1001-5965.2013.0756
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [1] A Dynamic Precision Evaluation Method for the Star Sensor in the Stellar-Inertial Navigation System
    Jiazhen Lu
    Chaohua Lei
    Yanqiang Yang
    Scientific Reports, 7
  • [2] A Dynamic Precision Evaluation Method for the Star Sensor in the Stellar-Inertial Navigation System
    Lu, Jiazhen
    Lei, Chaohua
    Yang, Yanqiang
    SCIENTIFIC REPORTS, 2017, 7
  • [3] Qualification of a New CVG-Based Inertial Reference Unit in a Combined Stellar-Inertial Attitude Determination System for Space Applications
    Schuh, F.
    Roessler, M.
    Haarlammert, T.
    Ahlendorf, F.
    Riedel, J.
    Groebel, J.
    Jacobs, T.
    Wolf, B.
    2018 DGON INERTIAL SENSORS AND SYSTEMS (ISS), 2018,
  • [4] Stellar inertial attitude determination for LEO spacecraft
    Wu, A
    Hein, DH
    PROCEEDINGS OF THE 35TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-4, 1996, : 3236 - 3244
  • [5] The Optical Reference Error Analysis and Control Method in Ground Validation System of Stellar-Inertial Integration
    Yang, Yanqiang
    Zhang, Chunxi
    Lu, Jiazhen
    Zhang, Hao
    IEEE SENSORS JOURNAL, 2019, 19 (02) : 670 - 678
  • [6] Strapdown stellar-inertial composite guidance method for ballistic missiles considering star sensor installation errors
    Zhao Y.
    Zhang H.
    Tang G.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2020, 41 (08):
  • [7] The inertial stellar compass: A multifunction, low power, attitude determination technology breakthrough
    Brady, T
    Buckley, S
    Dennehy, CJ
    Gambino, J
    Maynard, A
    GUIDANCE AND CONTROL 2003, 2003, 113 : 39 - 56
  • [8] Gyro-stellar inertial attitude estimation for satellite with high motion rate
    Lin, C-L
    Li, J-C
    Chiu, C-L
    Wu, Y-W A.
    Jan, Y-W
    AERONAUTICAL JOURNAL, 2022, 126 (1306): : 1967 - 1981
  • [9] Inertial/celestial-based method for satellite attitude determination
    Wang, Xiao-Chu
    Zhao, Kai-Chun
    You, Zheng
    Qinghua Daxue Xuebao/Journal of Tsinghua University, 2013, 53 (03): : 300 - 306
  • [10] A tracking method for GPS signal under high dynamic condition
    Kuang, Hong-Bo
    Mao, Xu-Chu
    Wang, Yong-Kai
    Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2012, 46 (06): : 854 - 858
12345