Calculating Transfer Families to Periodic Distant Retrograde Orbits Using Differential Correction

被引:13
|
作者
Scott, Christopher J. [1 ]
Spencee, David B. [1 ]
机构
[1] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
关键词
EXPLORATION;
D O I
10.2514/1.47791
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The existence of collision orbits in the vicinity of the distant retrograde region is well documented in works involving satellite capture. This study uses the orderly arrangement of collision regions and a dynamical analysis to calculate transfer families to periodic distant retrograde orbits. The work provides a systematic procedure to produce transfer families, providing an alternative to other methods and a framework in which to understand the design space.
引用
收藏
页码:1592 / 1605
页数:14
相关论文
共 27 条
  • [21] Low-cost transfer between asteroids with distant orbits using multiple gravity assists
    Yang, Hongwei
    Li, Jingyang
    Baoyin, Hexi
    ADVANCES IN SPACE RESEARCH, 2015, 56 (05) : 837 - 847
  • [22] Midcourse correction of Earth-Moon distant retrograde orbit transfer trajectories based on high-order state transition tensors
    Yongchen Yin
    Ming Wang
    Yu Shi
    Hao Zhang
    Astrodynamics, 2023, 7 : 335 - 349
  • [23] Midcourse correction of Earth-Moon distant retrograde orbit transfer trajectories based on high-order state transition tensors
    Yin, Yongchen
    Wang, Ming
    Shi, Yu
    Zhang, Hao
    ASTRODYNAMICS, 2023, 7 (03) : 335 - 349
  • [24] Precise halo orbit design and optimal transfer to halo orbits from earth using differential evolution
    Nath, Pranav
    Ramanan, R. V.
    ADVANCES IN SPACE RESEARCH, 2016, 57 (01) : 202 - 217
  • [25] Optimizing background correction when calculating differential renal function in the presence of hydroureteronephrosis using 99Tcm-DTPA
    Van de Wiele, C
    De Sadeleer, C
    Koole, M
    D'Asseler, Y
    Everaert, K
    Dierckx, RA
    NUCLEAR MEDICINE COMMUNICATIONS, 1998, 19 (03) : 251 - 255
  • [26] Analysis of Correction of the Trajectory of Launching a Spacecraft into High Circular Orbits of an Artificial Moon Satellite Using a Two-Impulse Transfer
    Gordienko, E. S.
    Ivashkin, V. V.
    COSMIC RESEARCH, 2024, 62 (05) : 519 - 532
  • [27] Investigation of near-rectilinear halo orbit search and rescue using staging L1 / L2 Lyapunov and distant retrograde orbit families
    Fay, Thomas J.
    Wilmer, Adam P.
    Bettinger, Robert A.
    JOURNAL OF SPACE SAFETY ENGINEERING, 2024, 11 (02): : 165 - 173