Optimal Multi-Impulse Orbit Transfer Using Nonlinear Relative Motion Dynamics

被引:0
|
作者
Weijun Huang
机构
[1] University of Missouri-Columbia,PhD student, Department of Mechanical and Aerospace Engineering
关键词
Transfer Problem; Initial Value Problem; State Transition Matrix; Standard Problem; Satellite Formation;
D O I
10.1007/s40295-013-0015-4
中图分类号
学科分类号
摘要
Trajectory planning for satellite formation flying missions requires the ability to find the optimal control law to transfer a satellite from one periodic relative orbit to another. This article modifies Jezewski’s linear impulsive trajectory optimization method for solving nonlinear problems described in the relative coordinate frame, and proposes the concept of standard problems for the initialization of the optimizer. With this modified optimizer and the standard problem concept, the article studies the impulse number, the cost, and the nonlinearity of fixed-time coplanar transfer problems.
引用
收藏
页码:237 / 258
页数:21
相关论文
共 50 条
  • [1] OPTIMAL MULTI-IMPULSE ORBIT TRANSFER USING NONLINEAR RELATIVE MOTION DYNAMICS
    Huang, Weijun
    [J]. KYLE T. ALFRIEND ASTRODYNAMICS SYMPOSIUM, 2011, 139 : 237 - 256
  • [2] Optimal Multi-Impulse Orbit Transfer Using Nonlinear Relative Motion Dynamics
    Huang, Weijun
    [J]. JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2012, 59 (1-2): : 243 - 264
  • [3] Optimal multi-impulse orbit transfer using nonlinear relative motion dynamics
    Department of Mechanical and Aerospace Engineering, University of Missouri-Columbia, E1412 Laffene Hall, Columbia, MO 65201, United States
    [J]. J Astronaut Sci, 2012, 1-2 (243-264):
  • [4] Fuel-Optimal Multi-Impulse Orbit Transfer Using a Hybrid Optimization Method
    Zhou, Hongyu
    Wang, Xiaogang
    Cui, Naigang
    [J]. IEEE TRANSACTIONS ON INTELLIGENT TRANSPORTATION SYSTEMS, 2020, 21 (04) : 1359 - 1368
  • [5] OPTIMAL MULTI-IMPULSE TRAJECTORIES
    MINKOFF, M
    LION, PM
    [J]. ASTRONAUTICA ACTA, 1969, 14 (04): : 359 - &
  • [6] Fuel optimal multi-impulse orbit rendezvous between neighboring orbits: A numerical approach
    No, TS
    [J]. ASTRODYNAMICS 1997, 1998, 97 : 707 - 718
  • [7] Algebraic Approach to the Minimum-Cost Multi-Impulse Orbit-Transfer Problem
    Avendano, M.
    Martin-Molina, V.
    Martin-Morales, J.
    Ortigas-Galindo, J.
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (08) : 1734 - 1743
  • [8] Regularizing fuel-optimal multi-impulse trajectories
    Kenta Oshima
    [J]. Astrodynamics, 2024, 8 : 97 - 119
  • [9] LINEARIZED THEORY OF OPTIMAL MULTI-IMPULSE ORBITAL TRANSFERS
    KUZMAK, GE
    LAVRENKO, NI
    [J]. JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1964, 11 (03): : 88 - &
  • [10] GAME PROBLEM OF THE DESIGN OF A MULTI-IMPULSE MOTION CORRECTION
    MELIKIAN, AA
    [J]. PMM JOURNAL OF APPLIED MATHEMATICS AND MECHANICS, 1980, 44 (05): : 555 - 560