Abstract
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.
| Original language | English |
|---|---|
| Title of host publication | SpaceOps 2016 Conference |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624104268 |
| DOIs | |
| Publication status | Published - 2016 Jan 1 |
| Event | 14th International Conference on Space Operations, SpaceOps 2016 - Daejeon, Korea, Republic of Duration: 2016 May 16 → 2016 May 20 |
Other
| Other | 14th International Conference on Space Operations, SpaceOps 2016 |
|---|---|
| Country | Korea, Republic of |
| City | Daejeon |
| Period | 16/5/16 → 16/5/20 |
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All Science Journal Classification (ASJC) codes
- Space and Planetary Science
- Aerospace Engineering
- Acoustics and Ultrasonics
Cite this
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Preliminary design of LUDOLP : The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission. / Song, Young Joo; Lee, Donghun; Bae, Jonghee; Kim, Bangyeop; Kim, Youngkwang; Lee, Eunji; Kim, Hyun Jeong; Park, Sang Young.
SpaceOps 2016 Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. AIAA 2016-2311.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
TY - GEN
T1 - Preliminary design of LUDOLP
T2 - The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission
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
BT - SpaceOps 2016 Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
ER -