The ground tracking support is a critical factor for the navigation performance of spacecraft orbiting around the Moon. Because of the tracking limit of antennas, only a small number of facilities can support lunar missions. Therefore, case studies for various ground tracking support conditions are needed for lunar missions on the stage of preliminary mission analysis. This study analyzes the ground supporting condition effect on orbit determination (OD) of Korea Pathfinder Lunar Orbiter (KPLO) in the lunar orbit. For the assumption of ground support conditions, daily tracking frequency, cut-off angle for low elevation, tracking measurement accuracy, and tracking failure situations were considered. Two antennas of deep space network (DSN) and Korea Deep Space Antenna (KDSA) are utilized for various tracking conditions configuration. For the investigation of the daily tracking frequency effect, three cases (full support, DSN 4 pass/day and KDSA 4 pass/day, and DSN 2 pass/day and KDSA 2 pass/day) are prepared. For the elevation cut-off angle effect, two situations, which are 5 deg and 10 deg, are assumed. Three cases (0%, 30%, and 50% of degradation) were considered for the tracking measurement accuracy effect. Three cases such as no missing, 1-day KDSA missing, and 2-day KDSA missing are assumed for tracking failure effect. For OD, a sequential estimation algorithm was used, and for the OD performance evaluation, position uncertainty, position differences between true and estimated orbits, and orbit overlap precision according to various ground supporting conditions were investigated. Orbit prediction accuracy variations due to ground tracking conditions were also demonstrated. This study provides a guideline for selecting ground tracking support levels and preparing a backup plan for the KPLO lunar mission phase.

1. INTRODUCTION
2. MEASUREMENT SIMULATION
3. ORBIT DETERMINATION
4. RESULTS
    4.1 Daily Tracking Frequency Effect
    4.2 Low Elevation Cut-off Angle Effect
    4.3 Tracking Accuracy Effect
    4.4 Tracking Failure Effect
5. CONCLUSIONS
REFERENCES

• Young-Rok Kim(Korea Aerospace Research Institute) Corresponding Author
• Young-Joo Song(Korea Aerospace Research Institute)
• Jae-ik Park(Korea Aerospace Research Institute)
• Donghun Lee(Korea Aerospace Research Institute)
• Jonghee Bae(Korea Aerospace Research Institute)
• SeungBum Hong(Korea Aerospace Research Institute)
• Dae-Kwan Kim(Korea Aerospace Research Institute)
• Sang-Ryool Lee(Korea Aerospace Research Institute)