A Guidance and Navigation Strategy for Rendezvous and Proximity Operations with a Noncooperative Spacecraft in Geosynchronous Orbit

被引:22
|
作者
Barbee, Brent W. [1 ]
Carpenter, J. Russell [1 ]
Heatwole, Scott [2 ]
Markley, F. Landis [1 ]
Moreau, Michael [1 ]
Naasz, Bo J. [1 ]
Van Eepoel, John [1 ]
机构
[1] NASA, Goddard Space Flight Ctr, Greenbelt, MD 20771 USA
[2] NASA, GSFCs, Wallops Flight Facil, Wallops Isl, VA 23337 USA
来源
JOURNAL OF THE ASTRONAUTICAL SCIENCES | 2011年 / 58卷 / 03期
关键词
Global Position System; Global Position System Receiver; Navigation Strategy; Relative Navigation; Target Spacecraft;
D O I
10.1007/BF03321176
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The feasibility and benefits of various spacecraft servicing concepts are currently being assessed, and all require that servicer spacecraft perform rendezvous, proximity operations, and capture operations with the spacecraft to be serviced. There are many high-value commercial and military spacecraft located in geosynchronous orbit (GEO) which may be candidates for servicing, but GEO is a regime in which rendezvous and capture operations are not commonplace; further, most GEO spacecraft were not designed to be cooperative rendezvous targets, and some may even be completely nonfunctional and therefore potentially tumbling. In this work we present elements of a guidance and navigation strategy for rendezvous and proximity operations with a noncooperative spacecraft in GEO. Translational Ay is assessed for a passively safe co-elliptic rendezvous approach sequence that is followed by injection into a safety ellipse about a noncooperative tumbling spacecraft and, ultimately, final approach to capture. Covariance analysis is presented for a simulation of range and bearing measurements throughout the rendezvous and proximity operations sequence.
引用
收藏
页码:389 / 408
页数:20
相关论文
共 50 条
  • [1] A Guidance and Navigation Strategy for Rendezvous and Proximity Operations with a Noncooperative Spacecraft in Geosynchronous Orbit
    Brent W. Barbee
    J. Russell Carpenter
    Scott Heatwole
    F. Landis Markley
    Michael Moreau
    Bo J. Naasz
    John Van Eepoel
    The Journal of the Astronautical Sciences, 2011, 58 : 389 - 408
  • [2] A Coupled Guidance & Navigation Optimization to Improve Rendezvous and Proximity Operations
    Petersen, Christopher
    AIAA SCITECH 2024 FORUM, 2024,
  • [3] Introducing the satellite dashboard: A tool for enhancing the visibility of rendezvous and proximity operations in geosynchronous orbit
    Simone, Nevan
    Weeden, Brian C.
    Jah, Moriba K.
    JOURNAL OF SPACE SAFETY ENGINEERING, 2022, 9 (02): : 251 - 256
  • [4] Guidance of micro-spacecraft for rendezvous with noncooperative target
    School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
    Hangkong Xuebao, 2009, 8 (1466-1471):
  • [5] Autonomous navigation and rendezvous of spacecraft in lunar orbit
    Mikrin E.A.
    Mikhailov M.V.
    Rozhkov S.N.
    Gyroscopy and Navigation, 2010, 1 (04) : 310 - 320
  • [6] Development of an integrated spacecraft Guidance, Navigation, & Control subsystem for automated proximity operations
    Schulte, Peter Z.
    Spencer, David A.
    ACTA ASTRONAUTICA, 2016, 118 : 168 - 186
  • [7] A Robust Monocular Line-based Relative Navigation Approach for Spacecraft Rendezvous and Proximity Operations
    Velentzas, Iason Georgios
    Dor, Mehregan
    Tsiotras, Panagiotis
    AIAA SCITECH 2024 FORUM, 2024,
  • [8] An Angles-Only Navigation and Control Scheme for Noncooperative Rendezvous Operations
    Zhang, Yizhai
    Huang, Panfeng
    Song, Kehao
    Meng, Zhongjie
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2019, 66 (11) : 8618 - 8627
  • [9] An Autonomous Rendezvous Navigation and Guidance Method in Mars Orbit
    Liu T.
    Xie Y.-C.
    Wang X.-L.
    Hu J.-C.
    Yuhang Xuebao/Journal of Astronautics, 2019, 40 (04): : 406 - 414
  • [10] Guidance and relative navigation for autonomous rendezvous in a circular orbit
    Hablani, HB
    Tapper, ML
    Dana-Bashian, DJ
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2002, 25 (03) : 553 - 562