Costate Scaling Method for Mayer-Form Multirendezvous Trajectory Optimization Problem-Reference-Cited by-同舟云学术

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Costate Scaling Method for Mayer-Form Multirendezvous Trajectory Optimization Problem

Published:2024-05 Issue:3 Volume:61 Page:878-888
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Guo Xiang¹^ORCID,Wu Di¹^ORCID,Jiang Fanghua¹

Affiliation:

1. Tsinghua University, 100084 Beijing, People’s Republic of China

Funder

National Key Research and Development Program of China

Postdoctoral Science Foundation of China

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A35857

Reference32 articles.

1. Artificial Neural Networks for Multiple NEA Rendezvous Missions with Continuous Thrust

2. Mission design for deep space 1: A low-thrust technology validation mission

3. Dawn: A mission in development for exploration of main belt asteroids Vesta and Ceres

4. Shape-Based Approach to Low-Thrust Rendezvous Trajectory Design

5. Optimal Control Problem for Low-Thrust Multiple Asteroid Tour Missions

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