Efficient optimization method for variable-specific-impulse low-thrust trajectories with shutdown constraint

被引:0
|
作者
JIA FeiDa [1 ,2 ]
QIAO Dong [1 ,2 ]
HAN HongWei [1 ,2 ]
LI XiangYu [1 ,2 ]
机构
[1] School of Aerospace Engineering, Beijing Institute of Technology
[2] Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information
关键词
D O I
暂无
中图分类号
V43 [推进系统(发动机、推进器)];
学科分类号
080703 ; 082502 ;
摘要
This paper develops a sequential convex programming(SCP)-based method to solve the minimum-fuel variable-specific-impulse low-thrust transfer problem considering shutdown constraint, with emphasize on improving the computational efficiency. The variable parameter engine is more applicable for many low-thrust scenarios, therefore, both a continuously variable model and a ladder variable model are adopted. First, the original problem is convexified by processing the constraint feasible domain, which is composed of the nonlinear dynamic equations and second-order equality constraint, into convex sets. Then, the approximation is generated to close the optimal solution of the low-thrust problem by iteratively solving the convexified subproblem. Moreover, the switching self-detection and adaptive node refinement methods are presented, which can improve the accuracy of the solution and accelerate the convergence during the approximation process and is especially necessary and effective in the scenarios with shutdown constraint. In numerical simulations, the comparison with the homotopic approach shows that the proposed method only needs 4% computational time as that of the homotopic approach, and two variable-specificimpulse examples further demonstrate the effectiveness and efficiency of the proposed method.
引用
收藏
页码:581 / 594
页数:14
相关论文
共 50 条
  • [21] INDIRECT OPTIMIZATION OF LOW-THRUST TRAJECTORIES USING HOMOTOPY
    Wall, Bradley
    SPACEFLIGHT MECHANICS 2019, VOL 168, PTS I-IV, 2019, 168 : 141 - 158
  • [22] INDIRECT OPTIMIZATION OF LOW-THRUST EARTH ESCAPE TRAJECTORIES
    Huang, Hao
    Gong, Qi
    Han, Chao
    SPACEFLIGHT MECHANICS 2013, PTS I-IV, 2013, 148 : 1523 - 1531
  • [23] Analytical gradient-based optimization method for low-thrust transfer trajectories
    Shang, Haibin
    Cui, Pingyuan
    Qiao, Dong
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2010, 31 (12): : 2365 - 2372
  • [24] LOW-THRUST ELLIPTIC SPIRAL TRAJECTORIES OF A SATELLITE OF VARIABLE MASS
    ECKSTEIN, MC
    SHI, YY
    AIAA JOURNAL, 1967, 5 (08) : 1491 - &
  • [25] APPROXIMATION OF CONSTRAINT LOW-THRUST SPACE TRAJECTORIES USING FOURIER SERIES
    Taheri, Ehsan
    Abdelkhalik, Ossama
    ASTRODYNAMICS 2011, PTS I - IV, 2012, 142 : 2365 - 2384
  • [26] The Method of Linearization in Optimization Problems of Low-Thrust Spacecraft Trajectories: Optimal Nodes Layout
    Kazmerchuk, P. V.
    Vernigora, L. V.
    SOLAR SYSTEM RESEARCH, 2022, 56 (07) : 521 - 526
  • [27] An approach to design and optimization of low-thrust trajectories with gravity assists
    McConaghy, TT
    Debban, TJ
    Petropoulos, AE
    Longuski, JM
    ASTRODYNAMICS 2001, PTS I-III, 2001, 109 : 2337 - 2355
  • [28] Practical Method for Optimization of Low-Thrust Transfers
    Gil-Fernandez, Jesus
    Gomez-Tierno, Miguel A.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (06) : 1927 - 1931
  • [29] The Method of Linearization in Optimization Problems of Low-Thrust Spacecraft Trajectories: Optimal Nodes Layout
    P. V. Kazmerchuk
    L. V. Vernigora
    Solar System Research, 2022, 56 : 521 - 526
  • [30] THRUST OPTIMIZATION OF A NUCLEAR ROCKET OF VARIABLE SPECIFIC IMPULSE
    WANG, CJ
    ANTHONY, GW
    LAWRENCE, HR
    ARS JOURNAL, 1959, 29 (05): : 341 - 344