Fast preliminary design of low-thrust trajectories for multi-asteroid exploration-Reference-Cited by-同舟云学术

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Fast preliminary design of low-thrust trajectories for multi-asteroid exploration

Published:2019-10 Issue: Volume:93 Page:105295
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Fan Zichen,Huo Mingying,Qi Naiming,Xu Ye,Song Zhiguo

Funder

National Natural Science Foundation of China

Shanghai Academy of Spaceflight Technology

China Postdoctoral Science Foundation

Heilongjiang Postdoctoral Fund

Harbin Institute of Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Multiobjective trajectory optimization for a suborbital spaceplane using directed search domain approach;Wang;Aerosp. Sci. Technol.,2018

2. Improved shaping approach to the preliminary design of low-thrust trajectories;Novak;J. Guid. Control Dyn.,2011

3. Survey of numerical methods for trajectory optimization;Betts;J. Guid. Control Dyn.,1998

4. Parameter estimation for optimal asteroid transfer trajectories using supervised machine learning;Shang;Aerosp. Sci. Technol.,2018

5. Analytical solution of the optimal steering law for non-ideal solar sail;Niccolai;Aerosp. Sci. Technol.,2017

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1. Initial trajectory design of low-thrust spacecraft considering attitude constraints;Scientific Reports;2024-08-30

2. Enhanced Finite Fourier Series for Low-Thrust Trajectory design;AIAA SCITECH 2024 Forum;2024-01-04

3. Rapid Trajectory Optimization of Continuous-Low-Thrust Spacecraft Based on Bezier Shape Function and Inverse Dynamics;Springer Aerospace Technology;2024

4. Initial Identification of Thrust and Orbit Elements for Continuous Thrust Spacecraft in Circular Orbit;Aerospace;2023-12-01

5. Robust estimation of distribution algorithms via fitness landscape analysis for optimal low-thrust orbital maneuvers;Applied Soft Computing;2023-09

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