Arc Second Pointing System of Near Space Observatories WASP
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摘要: WASP (Wallops Arc Second Pointer)是由美国国家航空航天局(NASA)开发的一种临近空间天文台亚角秒级指向系统, 旨在构建可适配多类科学载荷的临近空间天文观测平台. WASP系统由指向控制系统(PCS)和星跟踪器子系统(CARDS)组成, 该系统结合精密机械和电子组件, 辅以超压气球技术, 能在临近空间执行长时飞行任务, 同时保持亚角秒级的指向精度. WASP系统的灵活性和标准化设计使其能够适配多种科学载荷, 满足不同的任务需求. 在空间科学领域, WASP系统的应用不仅拓宽了高空科学气球的研究范围, 也为临近空间天文台的建设提供了创新方案, 推动了对临近空间的探索. WASP系统的成功试飞和应用, 为其在行星科学、天体物理学和地球观测等领域的应用奠定了基础, 也为中国临近空间科学的发展提供了可靠的参考.Abstract: The Wallops Arc Second Pointer (WASP), developed by the National Aeronautics and Space Administration (NASA) in response to the challenge of sub-arcsecond-level pointing stability for high-altitude scientific balloon platforms during long-duration observational missions, is a near-space observatory-grade sub-arcsecond pointing system designed to establish a multi-payload-compatible near-space astronomical observation platform. Comprising a Pointing Control System (PCS) and a star tracker subsystem (Camera Attitude Reference Determination System, CARDS), WASP serves as the core technology for achieving high-precision fine-pointing control in near-space environments. By integrating precision mechanical and electronic components with super-pressure balloon technology, the system enables extended-duration missions in near-space while maintaining sub-arcsecond-level pointing accuracy. Its modular design and standardized interfaces allow seamless adaptation to diverse scientific payloads, fulfilling varied mission requirements. To transition early-stage ground-test hardware and software from laboratory settings to real-world flight conditions, the WASP team collaborated with multiple research groups to conduct five successive test flights. These flights validated the system's technical methodologies and performance capabilities while enabling further optimizations based on operational mission requirements. Following the completion of WASP’s development phase, the system has engaged in scientific collaborations with numerous research teams, producing notable achievements. Since 2014, WASP has supported missions including the X-Calibur hard X-ray polarimeter, BITSE (Balloon-borne Investigation of Temperature and Speed of Electrons in the corona), PICTURE-C (Planetary Imaging Concept Testbed Using a Recoverable Experiment-Coronagraph), SuperHERO (Super High-Energy Resolution Observatory), and XL-Calibur, yielding groundbreaking scientific results across astrophysics and planetary science domains. In the field of space science, WASP not only expands the research scope of high-altitude balloon platforms but also provides innovative solutions for constructing near-space observatories, advancing the exploration of near-space environments. The successful test flights and operational deployments of WASP have laid a foundation for its applications in planetary science, astrophysics, and Earth observation, while offering a reliable reference for the development of near-space science in China.
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表 1 5次试飞测试中的优化内容
Table 1. Optimizations made during 5 test flights
优化点 具体作用 试飞阶段 集成星追踪器 集成星追踪器到控制系统, 提高了指向精度和稳定性 技术验证飞行 电子设备位置调整 将航电甲板从外部框架移动到模拟望远镜上, 优化重量分布和空间利用 技术验证飞行 WASP轮毂编码器 在WASP轮毂上增加角度位置编码器, 提高了角度测量的精度 技术验证飞行 目标跟踪方案 在控制软件中实施新的定位方案, 主动补偿滚动角度扰动, 提高了扫描操作 的准确性 搭载科研仪器试飞 机械结构 修改冷却器的安装方式以提高隔离性, 并增加加强件以减少结构偏转 搭载科研仪器试飞 集成CARDS子系统 提供低成本系统, 为WASP控制系统提供姿态输入 搭载科研仪器试飞 集成三轴光纤陀螺仪 提供位置和加速度输出给WASP飞行计算机, 用于控制系统算法 搭载科研仪器试飞 动态平衡系统组件 使用动态平衡组件在飞行中补偿指向结构平衡的变化 搭载科研仪器试飞 自锁机构 提供冗余方法释放和锁定指向结构 搭载科研仪器试飞 集成星跟踪器 具有飞行中对齐目标和自主对准的能力 搭载科研仪器试飞 表 2 中国科学院临近空间球载天文台姿控吊舱研制目标
Table 2. Development objectives of the attitude control gondola for the near-space balloon-borne observatory by the Chinese Academy of Sciences
指向目标 应用场景 指向精度要求 对星定向 天文观测 ≤20″ 对日定向 太阳能电池标定 ≤0.3° -
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