Global Optimization of Multiple-Spacecraft Rendezvous Mission via Decomposition and Dynamics-Guide Evolution Approach
- 1 January 2022
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 45 (1), 171-178
- https://doi.org/10.2514/1.g006101
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (11972044)
This publication has 24 references indexed in Scilit:
- Multiple Space Debris Collecting Mission: Optimal Mission PlanningJournal of Optimization Theory and Applications, 2015
- Active debris multi-removal mission concept based on hybrid propulsionActa Astronautica, 2014
- Space debris selection and optimal guidance for removal in the SSO with low-thrust propulsionActa Astronautica, 2014
- Multispacecraft Refueling Optimization Considering the J2 Perturbation and Window ConstraintsJournal of Guidance, Control, and Dynamics, 2014
- Path optimization for Space Sweeper with Sling-Sat: A method of active space debris removalAdvances in Space Research, 2013
- Active debris removal: Recent progress and current trendsActa Astronautica, 2013
- Collision activities in the future orbital debris environmentAdvances in Space Research, 2005
- Analysis of J 2-perturbed motion using mean non-osculating orbital elementsCelestial Mechanics and Dynamical Astronomy, 2004
- SNOPT: An SQP Algorithm for Large-Scale Constrained OptimizationSIAM Journal on Optimization, 2002
- Collision frequency of artificial satellites: The creation of a debris beltJournal of Geophysical Research, 1978