Fast Trajectory Generation and Asteroid Sequence Selection in Multispacecraft for Multiasteroid Exploration

As an increasing number of asteroids are being discovered, detecting them using limited propulsion resources and time has become an urgent problem in the aerospace field. However, there is no universal fast asteroid sequence selection method that finds the trajectories for multiple low-thrust spacec...

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Veröffentlicht in:IEEE transactions on cybernetics 2022-07, Vol.52 (7), p.6071-6082
Hauptverfasser: Qi, Naiming, Fan, Zichen, Huo, Mingying, Du, Desong, Zhao, Ce
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container_issue 7
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container_title IEEE transactions on cybernetics
container_volume 52
creator Qi, Naiming
Fan, Zichen
Huo, Mingying
Du, Desong
Zhao, Ce
description As an increasing number of asteroids are being discovered, detecting them using limited propulsion resources and time has become an urgent problem in the aerospace field. However, there is no universal fast asteroid sequence selection method that finds the trajectories for multiple low-thrust spacecraft for detecting a large number of asteroids. Furthermore, the calculation efficiency of the traditional trajectory optimization method is low, and it requires a large number of iterations. Therefore, this study combines Monte Carlo tree search (MCTS) with spacecraft trajectory optimization. A fast MCTS pruning algorithm is proposed, which can quickly complete asteroid sequence selection and trajectory generation for multispacecraft exploration of multiple asteroids. By combining the Bezier shape-based (SB) method and MCTS, this study realizes the fast search of the exploration sequence and the efficient optimization of the continuous transfer trajectories. In the simulation example, compared with the traversal algorithm, the MCTS pruning algorithm obtained the global optimal detection sequence of the search tree in a very short time. Under the same conditions, the Bezier SB method obtained the transfer trajectory with a better performance index faster than the finite Fourier series SB method. Performances of the proposed method are illustrated through a complex asteroid multiflyby mission design.
doi_str_mv 10.1109/TCYB.2020.3040799
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subjects Acceleration
Algorithms
Asteroids
Bezier shape-based (SB) method
Exploration
Fourier series
low-thrust trajectory generation
Mission planning
Monte Carlo methods
Monte-Carlo tree search
multiasteroid exploration
multispacecraft
Optimization
Performance analysis
Performance indices
pruning algorithm
Search algorithms
Solar system
Space vehicles
Spacecraft
Spacecraft trajectories
Trajectory
Trajectory optimization
title Fast Trajectory Generation and Asteroid Sequence Selection in Multispacecraft for Multiasteroid Exploration
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