Spacecraft Single-Impulse Relative Reachable Domain in Earth-Centered, Earth-Fixed Coordinates-Reference-Cited by-同舟云学术

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Spacecraft Single-Impulse Relative Reachable Domain in Earth-Centered, Earth-Fixed Coordinates

Published:2024-09 Issue:9 Volume:47 Page:1991-2000
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Zhang Sai¹^ORCID,Yang Zhen¹^ORCID,Luo Ya-Zhong¹

Affiliation:

1. National University of Defense Technology, 410073 Changsha, People’s Republic of China

Funder

Technology Innovation Team of Manned Space Engineering

Young Elite Scientists Sponsorship Program

Natural Science Foundation of Hunan Province

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G008016

Reference26 articles.

1. Minimum Bounds on Multispacecraft ΔV Optimal Cooperative Rendezvous

2. Duality-Based Near-Fuel-Optimal Impulsive Trajectory Computation for Spacecraft Rendezvous Under Perturbations

3. Collision avoidance maneuver optimization with a multiple-impulse convex formulation

4. Orbital Accessibility Problem for Spacecraft with a Single Impulse

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