AEROSPACE SHANGHAI, Volume. 41, Issue 5, 113(2024)

Indirect Method of Energy-optimized Plane Trajectory Optimization for Electric Propulsion of Mars Orbit Insertion

Haiyang LI*... Xiaowen DUAN, Yingjie ZHAO, Tongjie LIU and Xi LU |Show fewer author(s)
Author Affiliations
  • Shanghai Institute of Satellite Engineering, Shanghai201109, China
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    References(13)

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    [13] F JIANG, G TANG, J LI. Improving low-thrust trajectory optimization by adjoint estimation with shape-based path. Journal of Guidance Control & Dynamics, 40, 3282-3289(2017).

    [14] H LI, H BAOYIN, F TOPPUTO. Neural networks in time-optimal low-thrust interplanetary transfers. IEEE Access, 7, 156413-156419(2019).

    [15] L CHENG, Z WANG, F JIANG et al. Fast generation of optimal asteroid landing trajectories using deep neural networks. IEEE Transactions on Aerospace and Electronic Systems, 56, 2642-2655(2019).

    [16] S CHEN, H LI, H BAOYIN. Multi-rendezvous low-thrust trajectory optimization using costate transforming and homotopic approach. Astrophysics and Space Science, 363, 128(2018).

    [17] H SHEN. No-guess indirect optimization of asteroid mission using electric propulsion. Optimal Control Applications and Methods, 39, 1061-1070(2018).

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    [26] S CARLETTA, M PONTANI, P TEOFILATTO. An earth-mars microsatellite mission leveraging low-energy capture and low-thrust propulsion. Acta Astronautica, 200, 635-646(2022).

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    Haiyang LI, Xiaowen DUAN, Yingjie ZHAO, Tongjie LIU, Xi LU. Indirect Method of Energy-optimized Plane Trajectory Optimization for Electric Propulsion of Mars Orbit Insertion[J]. AEROSPACE SHANGHAI, 2024, 41(5): 113

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    Paper Information

    Category: Innovation and Exploration

    Received: Feb. 23, 2024

    Accepted: --

    Published Online: Jan. 15, 2025

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2024.05.012

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