Collision probability based trajectory safety in close range guidance phase of rendezvous and docking

被引：0
|
作者：
College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, China [1 ]
机构：
来源：
Yuhang Xuebao | 2007年 / 3卷 / 648-652期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [1] Trajectory safety for close range guidance phase of rendezvous and docking
    College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
    Yuhang Xuebao/Journal of Astronautics, 2007, 28 (06): : 1554 - 1558
  • [2] Guidance Algorithm for the Final Translational Phase of Autonomous Close Range Rendezvous and Docking of Spacecraft
    Thomas, Maria
    Navin, M. S.
    Priya, Lal P. S.
    2015 INTERNATIONAL CONFERENCE ON CONTROL COMMUNICATION & COMPUTING INDIA (ICCC), 2015, : 143 - 148
  • [3] Collision probability based optimal collision avoidance maneuver in rendezvous and docking
    Wang, Hua
    Li, Hai-Yang
    Tang, Guo-Jin
    Yuhang Xuebao/Journal of Astronautics, 2008, 29 (01): : 220 - 223
  • [4] Pose Estimation and Trajectory Calculation for Autonomous Close-Range Rendezvous and Docking
    Priggemeyer, Marc
    Dimartino, Magdalena
    Rossmann, Juergen
    2015 IEEE/ASME INTERNATIONAL CONFERENCE ON ADVANCED INTELLIGENT MECHATRONICS (AIM), 2015, : 15 - 20
  • [5] Velocity-Free Guidance Scheme for Close-Range Rendezvous
    Shi, Xingwei
    Wang, Wei
    Lin, Defu
    Ji, Yi
    2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2018,
  • [6] Robust trajectory design and guidance for far-range rendezvous using reinforcement learning with safety and observability considerations
    Wijayatunga, Minduli Charithma
    Armellin, Roberto
    Holt, Harry
    AEROSPACE SCIENCE AND TECHNOLOGY, 2025, 159
  • [7] Asteroid Approach Guidance Based on Predicted Rendezvous Probability
    Zhu, Shengying
    Sui, Zhihui
    Jing, Yujie
    Xiu, Yi
    Ge, Dantong
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2025, 61 (01) : 684 - 695
  • [8] Closed Loop Guidance During Close Range Rendezvous in a Three Body Problem
    Galullo, Michele
    Bucchioni, Giordana
    Franzini, Giovanni
    Innocenti, Mario
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2022, 69 (01): : 28 - 50
  • [9] Closed Loop Guidance During Close Range Rendezvous in a Three Body Problem
    Michele Galullo
    Giordana Bucchioni
    Giovanni Franzini
    Mario Innocenti
    The Journal of the Astronautical Sciences, 2022, 69 : 28 - 50
  • [10] Spacecraft rendezvous trajectory safety quantitative performance index eliminating probability dilution
    SUN ZhenJiang
    LUO YaZhong
    NIU ZhiYong
    Science China(Technological Sciences), 2014, (06) : 1219 - 1228
12345