基于模糊预测控制策略的空间探测器能量管理

IF 2.8 3区 地球科学 Q2 ASTRONOMY & ASTROPHYSICS
Yuan Jiang , Zhan Lei , Liying Zhu , Shuo Liu , Suliang Ma
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引用次数: 0

摘要

有效控制电力推进和电池充放电电流是空间探测器能量管理的关键。提出了一种基于模糊预测控制(FMPC)算法的两级能量管理策略。首先,在上层决策层,初步确定电力推进的运行水平。采用模糊规则对电池健康状态(SOH)进行评估,指导电池的充放电方式,修改电力推进系统的运行水平。其次,在低层控制层,建立了电池的离散状态空间模型。利用二次规划控制电池电流,确保电力推进和其他负载的稳定能量供应。仿真结果表明,采用FMPC策略后,电池的过充过放时间减少23%,电池容量退化减少12.5%,电池寿命延长13%。电池电流也表现出良好的跟踪性能,最大瞬态偏差率仅为4%。最后进行了硬件在环测试。实验结果表明,与实验前期相比,由于较低的荷电状态(SOC),电力推进在后期的功率水平较低。电池电流跟踪偏差率保持在5%左右。空间探测器动力系统的功率分配和跟踪性能令人满意,验证了FMPC策略的可行性和有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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.
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来源期刊
Advances in Space Research
Advances in Space Research 地学天文-地球科学综合
CiteScore
5.20
自引率
11.50%
发文量
800
审稿时长
5.8 months
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.
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