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

Research output: Chapter in Book/Report/Conference proceedingConference 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 languageEnglish
Title of host publication14th International Conference on Space Operations
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624104268
Publication statusPublished - 2016 Jan 1
Event14th International Conference on Space Operations, 2016 - Daejeon, Korea, Republic of
Duration: 2016 May 162016 May 20

Publication series

Name14th International Conference on Space Operations, 2016

Other

Other14th International Conference on Space Operations, 2016
CountryKorea, Republic of
CityDaejeon
Period16/5/1616/5/20

Fingerprint

lunar flight
Lunar Orbiter
Lunar missions
Flight dynamics
Korea
flight
computer programs
software
Orbits
systems management
orbit determination
deep space
Earth orbits
space exploration
data simulation
maneuvers
prediction
predictions
mars
planning

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Song, Y. J., Lee, D., Bae, J., Kim, B., Kim, Y., Lee, E., ... 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.
Song, Young Joo ; Lee, Donghun ; Bae, Jonghee ; Kim, Bangyeop ; Kim, Youngkwang ; Lee, Eunji ; Kim, Hyun Jeong ; Park, Sang-Young. / Preliminary design of LUDOLP : The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission. 14th International Conference on Space Operations. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (14th International Conference on Space Operations, 2016).
@inproceedings{cb024202cddf42359fd708fd7454d6e2,
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’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.",
author = "Song, {Young Joo} and Donghun Lee and Jonghee Bae and Bangyeop Kim and Youngkwang Kim and Eunji Lee and Kim, {Hyun Jeong} and Sang-Young Park",
year = "2016",
month = "1",
day = "1",
language = "English",
isbn = "9781624104268",
series = "14th International Conference on Space Operations, 2016",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "14th International Conference on Space Operations",

}

Song, YJ, Lee, D, Bae, J, Kim, B, Kim, Y, Lee, E, Kim, HJ & 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, 14th International Conference on Space Operations, 2016, Daejeon, Korea, Republic of, 16/5/16.

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.

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 proceedingConference 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=84980009945&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84980009945&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84980009945

SN - 9781624104268

T3 - 14th International Conference on Space Operations, 2016

BT - 14th International Conference on Space Operations

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

ER -

Song YJ, Lee D, Bae J, Kim B, Kim Y, Lee E et al. Preliminary design of LUDOLP: The flight dynamics subsystem for the Korea pathfinder lunar orbiter mission. In 14th International Conference on Space Operations. American Institute of Aeronautics and Astronautics Inc, AIAA. 2016. (14th International Conference on Space Operations, 2016).