Yuan Jiang , Zhan Lei , Liying Zhu , Shuo Liu , Suliang Ma
{"title":"基于模糊预测控制策略的空间探测器能量管理","authors":"Yuan Jiang , Zhan Lei , Liying Zhu , Shuo Liu , Suliang Ma","doi":"10.1016/j.asr.2025.02.018","DOIUrl":null,"url":null,"abstract":"<div><div>Effective control of the electric propulsion and the charge–discharge current of the battery is crucial in energy management for space probes. A two-level energy management strategy based on a Fuzzy-Model Predictive Control (FMPC) algorithm is proposed in present work. First, in the upper-level, decision layer, the operating level of the electric propulsion is preliminarily determined. Fuzzy rules are employed to assess state of health (SOH) of the battery, guiding the charge–discharge modes and modifying the operating level of electric propulsion. Second, in the lower-level, control layer, a discretized state-space model of the battery is established. Using quadratic programming, the battery current is controlled to ensure a stable energy supply to both the electric propulsion and the other loads. Simulation results indicate that by applying the FMPC strategy, the over-charge or over-discharge time is reduced by 23 %, and the battery capacity degradation is decreased by 12.5 %, and the battery life is extended by 13 %. The battery current also shows good tracking performance, with a maximum transient deviation rate of only 4 %. Finally, hardware-in-the-loop tests are conducted. The experimental results demonstrate that, the electric propulsion operates at a lower power level in the later stages compared to the early stages of the experiment due to a lower state of charge (SOC). The battery current tracking deviation rate is maintained around 5 %. The power distribution and tracking performance of the power system of the space probe are satisfactory, validating the feasibility and effectiveness of the FMPC strategy.</div></div>","PeriodicalId":50850,"journal":{"name":"Advances in Space Research","volume":"75 8","pages":"Pages 6104-6117"},"PeriodicalIF":2.8000,"publicationDate":"2025-02-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Energy management of space probe based on fuzzy-model predictive control strategy\",\"authors\":\"Yuan Jiang , Zhan Lei , Liying Zhu , Shuo Liu , Suliang Ma\",\"doi\":\"10.1016/j.asr.2025.02.018\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Effective control of the electric propulsion and the charge–discharge current of the battery is crucial in energy management for space probes. A two-level energy management strategy based on a Fuzzy-Model Predictive Control (FMPC) algorithm is proposed in present work. First, in the upper-level, decision layer, the operating level of the electric propulsion is preliminarily determined. Fuzzy rules are employed to assess state of health (SOH) of the battery, guiding the charge–discharge modes and modifying the operating level of electric propulsion. Second, in the lower-level, control layer, a discretized state-space model of the battery is established. Using quadratic programming, the battery current is controlled to ensure a stable energy supply to both the electric propulsion and the other loads. Simulation results indicate that by applying the FMPC strategy, the over-charge or over-discharge time is reduced by 23 %, and the battery capacity degradation is decreased by 12.5 %, and the battery life is extended by 13 %. The battery current also shows good tracking performance, with a maximum transient deviation rate of only 4 %. Finally, hardware-in-the-loop tests are conducted. The experimental results demonstrate that, the electric propulsion operates at a lower power level in the later stages compared to the early stages of the experiment due to a lower state of charge (SOC). The battery current tracking deviation rate is maintained around 5 %. The power distribution and tracking performance of the power system of the space probe are satisfactory, validating the feasibility and effectiveness of the FMPC strategy.</div></div>\",\"PeriodicalId\":50850,\"journal\":{\"name\":\"Advances in Space Research\",\"volume\":\"75 8\",\"pages\":\"Pages 6104-6117\"},\"PeriodicalIF\":2.8000,\"publicationDate\":\"2025-02-12\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Advances in Space Research\",\"FirstCategoryId\":\"89\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0273117725001371\",\"RegionNum\":3,\"RegionCategory\":\"地球科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ASTRONOMY & ASTROPHYSICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Space Research","FirstCategoryId":"89","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0273117725001371","RegionNum":3,"RegionCategory":"地球科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ASTRONOMY & ASTROPHYSICS","Score":null,"Total":0}
Energy management of space probe based on fuzzy-model predictive control strategy
Effective control of the electric propulsion and the charge–discharge current of the battery is crucial in energy management for space probes. A two-level energy management strategy based on a Fuzzy-Model Predictive Control (FMPC) algorithm is proposed in present work. First, in the upper-level, decision layer, the operating level of the electric propulsion is preliminarily determined. Fuzzy rules are employed to assess state of health (SOH) of the battery, guiding the charge–discharge modes and modifying the operating level of electric propulsion. Second, in the lower-level, control layer, a discretized state-space model of the battery is established. Using quadratic programming, the battery current is controlled to ensure a stable energy supply to both the electric propulsion and the other loads. Simulation results indicate that by applying the FMPC strategy, the over-charge or over-discharge time is reduced by 23 %, and the battery capacity degradation is decreased by 12.5 %, and the battery life is extended by 13 %. The battery current also shows good tracking performance, with a maximum transient deviation rate of only 4 %. Finally, hardware-in-the-loop tests are conducted. The experimental results demonstrate that, the electric propulsion operates at a lower power level in the later stages compared to the early stages of the experiment due to a lower state of charge (SOC). The battery current tracking deviation rate is maintained around 5 %. The power distribution and tracking performance of the power system of the space probe are satisfactory, validating the feasibility and effectiveness of the FMPC strategy.
期刊介绍:
The COSPAR publication Advances in Space Research (ASR) is an open journal covering all areas of space research including: space studies of the Earth''s surface, meteorology, climate, the Earth-Moon system, planets and small bodies of the solar system, upper atmospheres, ionospheres and magnetospheres of the Earth and planets including reference atmospheres, space plasmas in the solar system, astrophysics from space, materials sciences in space, fundamental physics in space, space debris, space weather, Earth observations of space phenomena, etc.
NB: Please note that manuscripts related to life sciences as related to space are no more accepted for submission to Advances in Space Research. Such manuscripts should now be submitted to the new COSPAR Journal Life Sciences in Space Research (LSSR).
All submissions are reviewed by two scientists in the field. COSPAR is an interdisciplinary scientific organization concerned with the progress of space research on an international scale. Operating under the rules of ICSU, COSPAR ignores political considerations and considers all questions solely from the scientific viewpoint.