Abstract

The orbital characteristics of low Earth orbit (LEO) satellite systems prevent continuous monitoring because ground access time is limited. For this reason, the development of simulators for predicting satellite states for the entire orbit is required. Power-related prediction is one of the important LEO satellite simulations because it is directly related to the lifespan and mission of the satellite. Accurate predictions of the charge and discharge current of a power system’s battery are essential for fault management design, mission design, and expansion of LEO satellites. However, it is difficult to accurately predict the battery power demand and charging of LEO satellites because they have nonlinear characteristics that depend on the satellite’s attitude, season, orbit, mission, and operating period. Therefore, this paper proposes a novel battery charge and discharge current prediction technique using the bidirectional long short-term memory (Bi-LSTM) model for the development of a LEO satellite power simulator. The prediction performance is demonstrated by applying the proposed technique to the KOM-SAT-3A and KOMSAT-5 satellites operating in real orbits. As a result, the prediction accuracy of the proposed Bi-LSTM shows root mean square error (RMSE) within 2.3 A, and the prediction error well outperforms the most recent the probability-based SARIMA model.

Highlights

  • Monitoring the status of low Earth orbit (LEO) satellites is limited because of limited ground access time due to the non-contact duration in orbit

  • Power system simulators are critical because the power system is responsible for generating, distributing, and storing energy for the operation of the satellite, and it is closely related to the mission design, satellite lifespan, and fault management [1,2]

  • Mission and error management designs must ensure that the batteries used for LEO satellites are in the operating range that guarantees expected performance of the satellite [3,4]

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Summary

Introduction

Monitoring the status of LEO satellites is limited because of limited ground access time due to the non-contact duration in orbit. Power system simulators are critical because the power system is responsible for generating, distributing, and storing energy for the operation of the satellite, and it is closely related to the mission design, satellite lifespan, and fault management [1,2]. Because LEO satellites have limited communication with ground stations, it is necessary to predict the power state, including the non-contact duration. Such state prediction varies depending on the operating period, season, attitude, and mission of the satellite [5,6,7], which makes its mathematical modeling difficult

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