Low-energy Earth-Moon transfers via Theory of Functional Connections and homotopy

被引:1
作者
Campana, C. T. [1 ]
Merisio, G. [1 ]
Topputo, F. [1 ]
机构
[1] Politecn Milan, Dept Aerosp Sci & Technol, Via G La Masa 34, I-20156 Milan, Italy
关键词
Nonlinear astrodynamics; Earth-Moon transfers; High-fidelity trajectory design; Theory of Functional Connections; Homotopy continuation; WEAK STABILITY BOUNDARY; LIBRATION POINTS; PERIODIC-ORBITS; DESIGN; OPTIMIZATION; DYNAMICS;
D O I
10.1007/s10569-024-10192-5
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
Numerous missions leverage the weak stability boundary in the Earth-Moon-Sun system to achieve a safe and cost-effective access to the lunar environment. These transfers are envisaged to play a significant role in upcoming missions. This paper proposes a novel method to design low-energy transfers by combining the recent Theory of Functional Connections with a homotopic continuation approach. Planar patched transfer legs within the Earth-Moon and Sun-Earth systems are continued into higher-fidelity models. Eventually, the full Earth-Moon transfer is adjusted to conform to the dynamics of the planar Earth-Moon Sun-perturbed, bi-circular restricted four-body problem. The novelty lies in the avoidance of any propagation during the continuation process and final convergence. This formulation is beneficial when an extensive grid search is performed, automatically generating over 2000 low-energy transfers. Subsequently, these are optimized through a standard direct transcription and multiple shooting algorithm. This work illustrates that two-impulse low-energy transfers modeled in chaotic dynamic environments can be effectively formulated in Theory of Functional Connections, hence simplifying their overall design process. Moreover, its synergy with a homotopic continuation approach is demonstrated.
引用
收藏
页数:35
相关论文
共 38 条
  • [1] Allgower EL., 2003, INTRO NUMERICAL CONT, DOI [10.1137/1.9780898719154, DOI 10.1137/1.9780898719154]
  • [2] Multiobjective genetic optimization of Earth-Moon trajectories in the restricted four-body problem
    Assadian, Nima
    Pourtakdoust, Seid H.
    [J]. ADVANCES IN SPACE RESEARCH, 2010, 45 (03) : 398 - 409
  • [3] Weak Stability Boundary and Invariant Manifolds
    Belbruno, Edward
    Gidea, Marian
    Topputo, Francesco
    [J]. SIAM JOURNAL ON APPLIED DYNAMICAL SYSTEMS, 2010, 9 (03): : 1061 - 1089
  • [4] Survey of numerical methods for trajectory optimization
    Betts, JT
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1998, 21 (02) : 193 - 207
  • [5] Boyd J. P., 2000, CHEBYSHEV FOURIER SP
  • [6] Castelli R, 2011, NONLINEAR AND COMPLEX DYNAMICS: APPLICATIONS IN PHYSICAL, BIOLOGICAL, AND FINANCIAL SYSTEMS, P53, DOI 10.1007/978-1-4614-0231-2_4
  • [7] On the dynamics of weak stability boundary lunar transfers
    Circi, C
    Teofilatto, P
    [J]. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2001, 79 (01) : 41 - 72
  • [8] da Silva FS., 2012, J. Aerospace Eng. Sci. Appl, V4, P82, DOI [10.7446/jaesa.0401.08, DOI 10.7446/JAESA.0401.08]
  • [9] Rapid trajectory design in complex environments enabled by reinforcement learning and graph search strategies
    Das-Stuart, A.
    Howell, K. C.
    Folta, D. C.
    [J]. ACTA ASTRONAUTICA, 2020, 171 : 172 - 195
  • [10] Fast 2-impulse non-Keplerian orbit transfer using the Theory of Functional Connections
    de Almeida Junior, Allan K.
    Johnston, Hunter
    Leake, Carl
    Mortari, Daniele
    [J]. EUROPEAN PHYSICAL JOURNAL PLUS, 2021, 136 (02)