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

2 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	SpaceOps 2016 Conference
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	SpaceOps 2016 Conference

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

Funding Information:
This work was performed by the Korea Aerospace Research Institute (KARI) under a contract with the Ministry of Science, ICT and Future Planning (MSIP) through the ?Development of Pathfinder Lunar Orbiter and Key Technologies for the Second Stage Lunar Exploration? project (No. SR16023). The authors at Yonsei University were supported by the Core Space Technology Development Program of the National Research Foundation funded by the Korea Ministry of Science, ICT and Future Planning (NRF-2014M1A3A3A03034588).

Publisher Copyright:
© 2016 by Young-Joo Song, Donghun Lee, Jonghee Bae, Bangyeop Kim, Youngkwang Kim, Eunji Lee, Hyun-Jeong Kim and Sang-Young Park.

All Science Journal Classification (ASJC) codes

Space and Planetary Science
Aerospace Engineering
Acoustics and Ultrasonics

Access to Document

10.2514/6.2016-2311

Cite this

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 SpaceOps 2016 Conference [AIAA 2016-2311] (SpaceOps 2016 Conference). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2016-2311

@inproceedings{6840262b12ad4cfda5d84802be907543,

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}",

note = "Funding Information: This work was performed by the Korea Aerospace Research Institute (KARI) under a contract with the Ministry of Science, ICT and Future Planning (MSIP) through the ?Development of Pathfinder Lunar Orbiter and Key Technologies for the Second Stage Lunar Exploration? project (No. SR16023). The authors at Yonsei University were supported by the Core Space Technology Development Program of the National Research Foundation funded by the Korea Ministry of Science, ICT and Future Planning (NRF-2014M1A3A3A03034588). Publisher Copyright: {\textcopyright} 2016 by Young-Joo Song, Donghun Lee, Jonghee Bae, Bangyeop Kim, Youngkwang Kim, Eunji Lee, Hyun-Jeong Kim and Sang-Young Park.; 14th International Conference on Space Operations, SpaceOps 2016 ; Conference date: 16-05-2016 Through 20-05-2016",

year = "2016",

doi = "10.2514/6.2016-2311",

language = "English",

isbn = "9781624104268",

series = "SpaceOps 2016 Conference",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

booktitle = "SpaceOps 2016 Conference",

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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 SpaceOps 2016 Conference., AIAA 2016-2311, SpaceOps 2016 Conference, 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; 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 (SpaceOps 2016 Conference).

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

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AU - Kim, Bangyeop

AU - Kim, Youngkwang

AU - Lee, Eunji

AU - Kim, Hyun Jeong

AU - Park, Sang Young

N1 - Funding Information: This work was performed by the Korea Aerospace Research Institute (KARI) under a contract with the Ministry of Science, ICT and Future Planning (MSIP) through the ?Development of Pathfinder Lunar Orbiter and Key Technologies for the Second Stage Lunar Exploration? project (No. SR16023). The authors at Yonsei University were supported by the Core Space Technology Development Program of the National Research Foundation funded by the Korea Ministry of Science, ICT and Future Planning (NRF-2014M1A3A3A03034588). Publisher Copyright: © 2016 by Young-Joo Song, Donghun Lee, Jonghee Bae, Bangyeop Kim, Youngkwang Kim, Eunji Lee, Hyun-Jeong Kim and Sang-Young Park.

PY - 2016

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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

Y2 - 16 May 2016 through 20 May 2016

ER -

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

Abstract

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