OPTIMAL FINITE-THRUST RENDEZVOUS TRAJECTORIES FOUND VIA PARTICLE SWARM ALGORITHM

被引:0
|
作者
Pontani, Mauro [1 ]
Conway, Bruce A. [1 ]
机构
[1] Univ Roma La Sapienza, Scuola Ingn Aerosp, I-00138 Rome, Italy
来源
ASTRODYNAMICS 2011, PTS I - IV | 2012年 / 142卷
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The particle swarm optimization technique is a population-based stochastic method developed in recent years and successfully applied in several fields of research. It represents a very intuitive (and easy to program) methodology for global optimization, inspired by the behavior of bird flocks while searching for food. The particle swarm optimization technique attempts to take advantage of the mechanism of information sharing that affects the overall behavior of a swarm, with the intent of determining the optimal values of the unknown parameters of the problem under consideration. This research applies the technique to determining optimal continuous-thrust rendezvous trajectories in a rotating Euler-Hill frame. Hamiltonian methods are employed to translate the related optimal control problems into parameter optimization problems. Thus the parameters sought by the swarming algorithm are primarily the initial values of the costates and the final time. The algorithm at hand is extremely easy to program. Nevertheless, it proves to be effective, reliable, and numerically accurate in solving the rendezvous optimization problems considered in this work.
引用
收藏
页码:3781 / 3800
页数:20
相关论文
共 50 条
  • [1] Optimal Finite-Thrust Rendezvous Trajectories Found via Particle Swarm Algorithm
    Pontani, Mauro
    Conway, Bruce A.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2013, 50 (06) : 1222 - 1234
  • [2] Fuel-optimal trajectories for finite-thrust rendezvous
    Gu D.-K.
    Duan G.-R.
    Zhang M.-R.
    Yuhang Xuebao/Journal of Astronautics, 2010, 31 (01): : 75 - 81
  • [3] Indirect Optimization of Finite-Thrust Cooperative Rendezvous
    Zavoli, Alessandro
    Colasurdo, Guido
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (02) : 304 - 314
  • [4] High-accuracy optimal finite-thrust trajectories for Moon escape
    Shen, Hong-Xin
    Casalino, Lorenzo
    ACTA ASTRONAUTICA, 2017, 131 : 102 - 109
  • [5] Fuel-optimal finite-thrust space rendezvous based on mission planning
    Yan, Xun-Liang
    Tang, Yi-Hua
    Xu, Min
    Chen, Shi-Lu
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2010, 33 (06): : 611 - 615
  • [6] Optimal cooperative finite-thrust rendezvous based on hybrid optimization and multiple shooting method
    Pan, Wei
    Lu, Chang-Hou
    Feng, Wei-Ming
    Chen, Fei
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2010, 33 (06): : 603 - 610
  • [7] OPTIMAL FINITE-THRUST SPACECRAFT TRAJECTORIES USING COLLOCATION AND NONLINEAR-PROGRAMMING
    ENRIGHT, PJ
    CONWAY, BA
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1991, 14 (05) : 981 - 985
  • [8] Optimization of finite-thrust trajectories with fixed angular distance
    Petukhov, Viacheslav
    Ivanyukhin, Alexey
    Popov, Garri
    Testoyedov, Nikolay
    Yoon, Sung Wook
    ACTA ASTRONAUTICA, 2022, 197 : 354 - 367
  • [10] Optimal cooperative finite-thrust spacecraft out-of-plane rendezvous using direct collocation method
    Pan, Wei
    Lu, Chang-Hou
    Feng, Wei-Ming
    Ge, Pei-Qi
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2009, 32 (04): : 373 - 378