Optimal multi-segment trajectory of solar sail with analytical approximation

被引:0
|
作者
Qi, Ji [1 ]
Jin, Ruhao [1 ]
Zhao, Ce [1 ]
Gao, Zhibo [1 ]
Feng, Wenyu [1 ]
Fan, Zichen [1 ]
Huo, Mingying [1 ]
机构
[1] Harbin Inst Technol, Harbin 150001, Peoples R China
基金
中国国家自然科学基金; 美国国家科学基金会;
关键词
Solar sail; Analytical approximation; Multi-target exploration; Fixed pitch angle; LOW-THRUST; PRELIMINARY DESIGN; ELECTRIC SAIL;
D O I
10.1016/j.ast.2024.109384
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper focuses on the optimization of two-dimensional transfer trajectories for solar sails using analytical approximation and modified analytical approximation methods. Instead of assuming circular orbits [29-31,37], the proposed approach allows for the analysis of solar sails launched from general heliocentric elliptical orbits. By employing linear perturbation theory, analytical propelled trajectories with fixed pitch angles are derived, where the perturbation coefficient serves as the reference lightness coefficient. To obtain the optimal transfer orbit between general heliocentric elliptical orbits, the analytical segments corresponding to different pitch angles are spliced together. A nonlinear optimization algorithm is then utilized to optimize the multi-segment trajectory, aiming to achieve the optimal performance index while satisfying boundary and intermediate constraints. Remarkably, this method requires the optimization of only the pitch angle for each segment, resulting in a small number of optimization variables and significantly improved efficiency in transfer orbit optimization. Additionally, the analytical approximation approach offers substantial time savings compared to numerical integration, particularly when repeated calculations are involved. Furthermore, the modified approximate trajectory exhibits high accuracy, with the optimal analytical transfer trajectory closely approximating the optimal actual trajectory acquired through the shooting method. This paper extensively validates and analyzes the precision of the proposed analytical transfer orbit through numerical verification. Additionally, when contrasted with actual transfer orbit, the suggested analytical approach can significantly decrease the computation time for multi-object challenges by a minimum of 80%. This makes the proposed method highly suitable for rapid design of optimal transfer orbits in multi-target mission scenarios for solar sail-based probes.
引用
收藏
页数:10
相关论文
共 50 条
  • [21] TIME-OPTIMAL ORBIT TRANSFER TRAJECTORY FOR SOLAR SAIL SPACECRAFT
    JAYARAMAN, TS
    JOURNAL OF GUIDANCE AND CONTROL, 1980, 3 (06): : 536 - 542
  • [22] Solar sail time-optimal interplanetary transfer trajectory design
    Sheng-Ping Gong
    ResearchinAstronomyandAstrophysics, 2011, 11 (08) : 981 - 996
  • [23] Solar sail time-optimal interplanetary transfer trajectory design
    Gong, Sheng-Ping
    Gao, Yun-Feng
    Li, Jun-Feng
    RESEARCH IN ASTRONOMY AND ASTROPHYSICS, 2011, 11 (08) : 981 - 996
  • [24] Analytical Modeling of Multi-segment and Multilayer Interior Permanent Magnet Machines
    Zhu, Li
    Jiang, S. Z.
    Zhu, Z. Q.
    Chan, C. C.
    2014 17TH INTERNATIONAL CONFERENCE ON ELECTRICAL MACHINES AND SYSTEMS (ICEMS), 2014, : 28 - 33
  • [25] Multi-Segment Polynomial Trajectory Generation of Autonomous Vehicles Based on Quadratic Programming
    Wei, Chao
    Lv, Mo
    Ma, Benshan
    Zhang, Zhe
    Zhao, Botong
    Su, Menglun
    2024 4TH INTERNATIONAL CONFERENCE ON COMPUTER, CONTROL AND ROBOTICS, ICCCR 2024, 2024, : 171 - 177
  • [26] A multi-segment modelling approach for foot trajectory estimation using inertial sensors
    Okkalidis, Nikiforos
    Marinakis, George
    Gatt, Alfred
    Bugeja, Marvin K.
    Camilleri, Kenneth P.
    Falzon, Owen
    GAIT & POSTURE, 2020, 75 : 22 - 27
  • [27] Phasing multi-segment undulators
    Chavanne, J
    Elleaume, P
    VanVaerenbergh, P
    JOURNAL OF SYNCHROTRON RADIATION, 1996, 3 : 93 - 96
  • [28] Analytical Trajectory of Solar Sail With Fixed Pitch Angle From Elliptical Orbits
    Jin, Ruhao
    Fan, Zichen
    Huo, Mingying
    Xu, Ye
    Qi, Naiming
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2024, 60 (03) : 2833 - 2842
  • [29] Multi-segment steganography technique
    Alnawok, Fayik
    Ahmed, Basem
    INTERNATIONAL ARAB JOURNAL OF INFORMATION TECHNOLOGY, 2008, 5 (03) : 253 - 257
  • [30] Solar sail trajectory optimization of multi-asteroid rendezvous mission
    Song, Yu
    Gong, Shengping
    ACTA ASTRONAUTICA, 2019, 157 : 111 - 122