Practical Low-Thrust Geostationary Orbit Transfer Guidance via Linearized State Equations
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. Shanghai Institute of Satellite Engineering, 201109 Shanghai, People’s Republic of China
Funder
Beijing Natural Science Foundation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Reference29 articles.
1. Mission design for deep space 1: A low-thrust technology validation mission
2. Hayabusa—Its technology and science accomplishment summary and Hayabusa-2
3. Extension of Highly Elliptical Earth Orbits Using Continuous Low-Thrust Propulsion
4. Static, Highly Elliptical Orbits Using Hybrid Low-Thrust Propulsion
5. Sun-Synchronous Highly Elliptical Orbits Using Low-Thrust Propulsion
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2. Perturbed low-thrust geostationary orbit transfer guidance via polynomial costate estimation;Chinese Journal of Aeronautics;2023-10
3. Learning-Based Polynomial Approximation of Minimum-Time Low-Thrust Transfers to Geostationary Orbit;IEEE Transactions on Aerospace and Electronic Systems;2022
4. Optimization of low-thrust Earth-orbit transfers using the vectorial orbital elements;Aerospace Science and Technology;2021-05
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