TY - GEN
T1 - Preliminary design of LUDOLP
T2 - 14th International Conference on Space Operations, SpaceOps 2016
AU - Song, Young Joo
AU - Lee, Donghun
AU - Bae, Jonghee
AU - Kim, Bangyeop
AU - Kim, Youngkwang
AU - Lee, Eunji
AU - Kim, Hyun Jeong
AU - Park, Sang Young
PY - 2016/1/1
Y1 - 2016/1/1
N2 - The Korea Pathfinder Lunar Orbiter (KPLO), which is expected to launch in 2018 via international collaboration, will be the first Korean satellite to fly beyond Earth’s orbit. This work describes the preliminary design result of the lunar flight dynamics software for operational purpose (LUDOLP), the flight dynamics subsystem (FDS) of the KPLO mission. The system configuration of LUDOLP is discussed, including the details of each module’s functionalities, such as system management (SM), orbit determination (OD), orbit prediction (OP), event prediction (EP), maneuver planning and calibration (MPC), data simulation (DS) and fuel accounting (FA). The architecture of the ground segment (GS) for the KPLO mission is also briefly introduced. Building on the results of this study, the final version of LUDOLP will be developed in the near future to support the GS of the KPLO mission. The design of LUDOLP is expected to be directly applicable to Korea’s future deep space exploration missions to Mars and beyond.
AB - The Korea Pathfinder Lunar Orbiter (KPLO), which is expected to launch in 2018 via international collaboration, will be the first Korean satellite to fly beyond Earth’s orbit. This work describes the preliminary design result of the lunar flight dynamics software for operational purpose (LUDOLP), the flight dynamics subsystem (FDS) of the KPLO mission. The system configuration of LUDOLP is discussed, including the details of each module’s functionalities, such as system management (SM), orbit determination (OD), orbit prediction (OP), event prediction (EP), maneuver planning and calibration (MPC), data simulation (DS) and fuel accounting (FA). The architecture of the ground segment (GS) for the KPLO mission is also briefly introduced. Building on the results of this study, the final version of LUDOLP will be developed in the near future to support the GS of the KPLO mission. The design of LUDOLP is expected to be directly applicable to Korea’s future deep space exploration missions to Mars and beyond.
UR - http://www.scopus.com/inward/record.url?scp=85020549332&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85020549332&partnerID=8YFLogxK
U2 - 10.2514/6.2016-2311
DO - 10.2514/6.2016-2311
M3 - Conference contribution
AN - SCOPUS:85020549332
SN - 9781624104268
T3 - SpaceOps 2016 Conference
BT - SpaceOps 2016 Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
Y2 - 16 May 2016 through 20 May 2016
ER -