Design of All-Weather Celestial Navigation System

被引:0
作者
Sun Hongchi [1 ]
Mu Rongjun [1 ]
Du Huajun [2 ,3 ]
Wu Peng [1 ]
机构
[1] Harbin Inst Technol, Sch Astronautice, Harbin 150001, Heilongjiang, Peoples R China
[2] Beijing Aerosp Automat Control Inst, Beijing 100854, Peoples R China
[3] Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing 100854, Peoples R China
来源
YOUNG SCIENTISTS FORUM 2017 | 2018年 / 10710卷
关键词
Celestial navigation; Inertial navigation; Comentropy;
D O I
10.1117/12.2317547
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
In order to realize autonomous navigation in the atmosphere, an all-weather celestial navigation system is designed. The research of celestial navigation system include discrimination method of comentropy and the adaptive navigation algorithm based on the P value. The discrimination method of comentropy is studied to realize the independent switching of two celestial navigation modes, starlight and radio. Finally, an adaptive filtering algorithm based on P value is proposed, which can greatly improve the disturbance rejection capability of the system. The experimental results show that the accuracy of the three axis attitude is better than 10 '', and it can work all weather. In perturbation environment, the position accuracy of the integrated navigation system can be increased 20% comparing with the traditional method. It basically meets the requirements of the all-weather celestial navigation system, and it has the ability of stability, reliability, high accuracy and strong anti-interference.
引用
收藏
页数:8
相关论文
共 50 条
  • [21] Integrated Celestial Autonomous Navigation Method for Low Thrust Orbit Maneuver
    Ma G.-F.
    Wang W.
    Zhang W.
    Huang Q.-L.
    Peng Y.-M.
    Zhang X.
    Wang, Wei (deepspace509@126.com), 1600, China Spaceflight Society (41): : 1166 - 1174
  • [22] From the "arte de marear" (the art of seafaring) to celestial navigation: Navigation techniques and instruments in Spain of the modern era
    Gonzalez Gonzalez, Francisco Jose
    CUADERNOS DE HISTORIA MODERNA, 2006, : 135 - 166
  • [23] Autonomous celestial navigation method for a deep-space probe based on angle-constraint aided celestial angle measurement
    Huang, Yue-Qing
    Ma, Xin
    SCIENTIA SINICA-PHYSICA MECHANICA & ASTRONOMICA, 2022, 52 (01)
  • [24] Design of Multi-Sensor Integrated Navigation System for Helicopters
    Chen Shuai
    Han Yu
    Cao Fei
    Guan Xue-Yuan
    Gao Yu-Xia
    2011 30TH CHINESE CONTROL CONFERENCE (CCC), 2011, : 1987 - 1991
  • [25] Analysis of Ephemeris Errors in Autonomous Celestial Navigation during Mars Approach Phase
    Ning, Xiaolin
    Li, Zhuo
    Yang, Yuqing
    Fang, Jiancheng
    Liu, Gang
    JOURNAL OF NAVIGATION, 2017, 70 (03) : 505 - 526
  • [26] Differential X-ray pulsar aided celestial navigation for Mars exploration
    Ning, Xiaolin
    Gui, Mingzhen
    Fang, Jiancheng
    Liu, Gang
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 62 : 36 - 45
  • [27] Invariant Observer Design for a Helicopter UAV Aided Inertial Navigation System
    Barczyk, Martin
    Lynch, Alan F.
    IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2013, 21 (03) : 791 - 806
  • [28] Testing instrument design for inertial navigation system of a certain type of airplane
    Guo Chuang
    Yu Jin
    Pang Xinmin
    Proceedings of the First International Conference on Maintenance Engineering, 2006, : 460 - 465
  • [29] An Optimal Estimation Method for Multi-Velocity Vector Integration in Spacecraft Celestial Navigation
    You, Wei
    Ma, Guangfu
    Zhang, Wei
    2018 37TH CHINESE CONTROL CONFERENCE (CCC), 2018, : 4798 - 4802
  • [30] Research and Prospects on Celestial Integrated Navigation Methods for Deep Space Exploration of Jupiter and Beyond
    Zhang, Xiao
    Pan, Linxin
    Zhong, Yubin
    PROCEEDINGS OF THE 2024 3RD INTERNATIONAL SYMPOSIUM ON INTELLIGENT UNMANNED SYSTEMS AND ARTIFICIAL INTELLIGENCE, SIUSAI 2024, 2024, : 349 - 352