TY - JOUR
T1 - Low-Thrust Station-Keeping Strategy toward Exploiting the Resonances in the Geostationary Region
AU - Li, Lincheng
AU - Colombo, Camilla
AU - Gkolias, Ioannis
AU - Zhang, Jingrui
AU - Xu, Ming
N1 - Publisher Copyright:
© 2023 American Society of Civil Engineers.
PY - 2024/3/1
Y1 - 2024/3/1
N2 - Low-thrust propulsion systems are widely used in space missions due to their high specific impulse and reduced propellant consumption. However, current research focuses on eliminating drifts in low-thrust maneuvers, resulting in high operational costs for daily station-keeping. This study aims to achieve autonomous station-keeping by exploiting long-term periodic behaviors caused by geostationary resonances. First, resonance maps caused by the Earth's gravity and lunisolar perturbation are revisited. Then, station-keeping slots are selected based on a phase space study of the resonances. A closed station-keeping track is formed by designing a low-thrust arc to work with the drifting arc. This track moves along the edge of the station-keeping slot, providing a more extended control period and reducing ground-station operational costs. Finally, an indirect optimizing method and efficient initial costate guess technique are proposed for calculating low-thrust maneuvers.
AB - Low-thrust propulsion systems are widely used in space missions due to their high specific impulse and reduced propellant consumption. However, current research focuses on eliminating drifts in low-thrust maneuvers, resulting in high operational costs for daily station-keeping. This study aims to achieve autonomous station-keeping by exploiting long-term periodic behaviors caused by geostationary resonances. First, resonance maps caused by the Earth's gravity and lunisolar perturbation are revisited. Then, station-keeping slots are selected based on a phase space study of the resonances. A closed station-keeping track is formed by designing a low-thrust arc to work with the drifting arc. This track moves along the edge of the station-keeping slot, providing a more extended control period and reducing ground-station operational costs. Finally, an indirect optimizing method and efficient initial costate guess technique are proposed for calculating low-thrust maneuvers.
UR - http://www.scopus.com/inward/record.url?scp=85181102540&partnerID=8YFLogxK
U2 - 10.1061/JAEEEZ.ASENG-5330
DO - 10.1061/JAEEEZ.ASENG-5330
M3 - Article
AN - SCOPUS:85181102540
SN - 0893-1321
VL - 37
JO - Journal of Aerospace Engineering
JF - Journal of Aerospace Engineering
IS - 2
M1 - 04023123
ER -