Preliminary design of LUDOLP: The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission

Young Joo Song; Donghun Lee; Jonghee Bae; Bangyeop Kim; Youngkwang Kim; Eunji Lee; Hyun Jeong Kim; Sang Young Park

doi:10.2514/6.2016-2311

Preliminary design of LUDOLP: The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission

Young Joo Song, Donghun Lee, Jonghee Bae, Bangyeop Kim, Youngkwang Kim, Eunji Lee, Hyun Jeong Kim, Sang Young Park

Institute of Earth·Atmosphere·Astronomy(BK21+)

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

3 Citations (Scopus)

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	14th International Conference on Space Operations
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624104268
DOIs	https://doi.org/10.2514/6.2016-2311
Publication status	Published - 2016
Event	14th International Conference on Space Operations, SpaceOps 2016 - Daejeon, Korea, Republic of Duration: 2016 May 16 → 2016 May 20

Publication series

Name	14th International Conference on Space Operations, 2016

Other

Other	14th International Conference on Space Operations, SpaceOps 2016
Country/Territory	Korea, Republic of
City	Daejeon
Period	16/5/16 → 16/5/20

Bibliographical note

Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science

Access to Document

10.2514/6.2016-2311

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Song, Y. J., Lee, D., Bae, J., Kim, B., Kim, Y., Lee, E., Kim, H. J., & Park, S. Y. (2016). Preliminary design of LUDOLP: The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission. In 14th International Conference on Space Operations (14th International Conference on Space Operations, 2016). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2016-2311

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title = "Preliminary design of LUDOLP: The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission",

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{\textquoteright}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{\textquoteright}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{\textquoteright}s future deep space exploration missions to Mars and beyond.",

author = "Song, {Young Joo} and Donghun Lee and Jonghee Bae and Bangyeop Kim and Youngkwang Kim and Eunji Lee and Kim, {Hyun Jeong} and Park, {Sang Young}",

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year = "2016",

doi = "10.2514/6.2016-2311",

language = "English",

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Song, YJ, Lee, D, Bae, J, Kim, B, Kim, Y, Lee, E, Kim, HJ & Park, SY 2016, Preliminary design of LUDOLP: The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission. in 14th International Conference on Space Operations. 14th International Conference on Space Operations, 2016, American Institute of Aeronautics and Astronautics Inc, AIAA, 14th International Conference on Space Operations, SpaceOps 2016, Daejeon, Korea, Republic of, 16/5/16. https://doi.org/10.2514/6.2016-2311

Preliminary design of LUDOLP: The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission. / Song, Young Joo; Lee, Donghun; Bae, Jonghee et al.
14th International Conference on Space Operations. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (14th International Conference on Space Operations, 2016).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

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AU - Kim, Youngkwang

AU - Lee, Eunji

AU - Kim, Hyun Jeong

AU - Park, Sang Young

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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.

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PB - American Institute of Aeronautics and Astronautics Inc, AIAA

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ER -

Preliminary design of LUDOLP: The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission

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