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Taylor658/HET_Transfer_Orbit_Efficiency

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Hugging Face2024-06-03 更新2024-06-12 收录
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https://hf-mirror.com/datasets/Taylor658/HET_Transfer_Orbit_Efficiency
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--- title: "HET Transfer Orbit Efficiency Dataset" emoji: "🚀" description: "Data on the impact of space weather on Hall Effect Thrusters (HETs) efficiency, used in spacecraft transfer orbits" version: "1.0.2" license: "mit" tags: - "space weather" - "spacecraft" - "HETs" - "astronomy" - "physics" - "machine learning" language: - "en" annotations_creators: - "expert-generated" source_datasets: - "original" multilinguality: - "monolingual" size_categories: - "1K<n<10K" --- # HET Transfer Orbit Efficiency Dataset ## Overview This dataset encapsulates vital metrics relevant to understanding how space weather affects the operation and efficiency of Hall Effect Thrusters (HETs) used in spacecraft transfer orbits. These thrusters, which use noble gases, are crucial for precise maneuvering and station-keeping in space missions. ## Table of Contents - [Dataset Description](#dataset-description) - [Importance of Space Weather](#importance-of-space-weather) - [Data Fields](#data-fields) - [Usage Examples](#usage-examples) - [Additional Information](#additional-information) - [License](#license) ## Dataset Description The dataset comprises various parameters recorded during the operation of HETs operating in Transfer Orbits. Each entry is timestamped and includes measurements of magnetic fields, proton density, temperatures, and spacecraft coordinates — all factors influenced by space weather. ### Why Space Weather? Understanding space weather's effects on Hall Effect Thrusters (HETs) is crucial for: - **Thruster Performance**: Variations in plasma density and magnetic fields can directly affect thrust efficiency. - **Component Erosion**: Increased particle fluxes can accelerate wear on thruster components. - **Operational Stability**: Fluctuations in solar activity can impact the power systems that feed these thrusters. - **Mission Safety and Planning**: Protecting electronics from solar radiation and accurately planning trajectory adjustments are vital for mission success. ## Data Fields - `YYYY`: Year of data recording (converted to 2023 for consistency in examples) - `DOY`: Day of the year - `HR`: Hour of the day - `MN`: Minute of the hour - `Timeshift`: Time shift in seconds - `BX`: Magnetic field component in nanoTesla (nT) - `Proton Density`: Density of protons per cubic centimeter (n/cc) - `Temperature`: Temperature in Kelvin - `X(s/c), Y(s/c), Z(s/c)`: Spacecraft coordinates in GSE coordinate system (in Earth Radii, Re) ### Example Data ```plaintext | YYYY | DOY | HR | MN | Timeshift | BX | Proton Density | Temperature | X(s/c) | Y(s/c) | Z(s/c) | |------|-----|----|----|-----------|------|----------------|-------------|--------|--------|--------| | 2023 | 1 | 4 | 6 | 1513 | 0.38 | 999.99 | 9999999. | 9999.99| 9999.99| 9999.99| | 2023 | 1 | 4 | 27 | 1526 | 0.13 | 6.77 | 164280. | 197.11 | 55.25 | -11.39 | ``` ## Usage Examples Here's how you might use this dataset in a Python script: ```python import pandas as pd data = pd.read_csv('het_data.csv') print(data.head()) ``` ## Additional Information For further queries or if you wish to contribute to or extend this dataset, please reach out through the repository's author ## License This dataset is made available under the MIT License. For more details, see the LICENSE file included with the dataset.
提供机构:
Taylor658
原始信息汇总

HET Transfer Orbit Efficiency Dataset 概述

数据集基本信息

  • 标题: HET Transfer Orbit Efficiency Dataset
  • 描述: 该数据集记录了空间天气对用于航天器转移轨道的霍尔效应推进器(HETs)效率的影响。
  • 版本: 1.0.2
  • 许可证: MIT
  • 标签: 空间天气, 航天器, HETs, 天文学, 物理学, 机器学习
  • 语言: 英语
  • 注释创建者: 专家生成
  • 数据来源: 原始数据
  • 多语言性: 单语
  • 大小类别: 1K<n<10K

数据集内容

数据描述

  • 包含参数: 数据集记录了HETs在转移轨道运行期间的多种参数,包括磁场、质子密度、温度和航天器坐标等,这些参数均受空间天气影响。
  • 时间戳: 每个数据条目都带有时间戳。

数据字段

  • YYYY: 数据记录年份(统一转换为2023年)
  • DOY: 一年中的第几天
  • HR: 一天中的小时
  • MN: 小时中的分钟
  • Timeshift: 时间偏移,单位为秒
  • BX: 磁场分量,单位为纳特斯拉(nT)
  • Proton Density: 质子密度,单位为每立方厘米的粒子数(n/cc)
  • Temperature: 温度,单位为开尔文
  • X(s/c), Y(s/c), Z(s/c): 航天器坐标,单位为地球半径(Re),采用地心太阳同步坐标系统(GSE)

示例数据

plaintext

YYYY DOY HR MN Timeshift BX Proton Density Temperature X(s/c) Y(s/c) Z(s/c)
2023 1 4 6 1513 0.38 999.99 9999999. 9999.99 9999.99 9999.99
2023 1 4 27 1526 0.13 6.77 164280. 197.11 55.25 -11.39

数据集用途

  • 推进器性能分析: 分析等离子体密度和磁场变化对推进效率的影响。
  • 组件磨损评估: 评估粒子通量增加对推进器组件磨损的影响。
  • 操作稳定性研究: 研究太阳活动波动对供电系统的影响。
  • 任务安全与规划: 保护电子设备免受太阳辐射,精确规划轨迹调整。
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