海洋盐度探测卫星控制分系统设计与在轨验证

AOCS Design and On-orbit Verification of Sea Surface Salinity Satellite

  • 摘要: 海洋盐度探测卫星是我国首颗用于观测海洋盐度的海洋动力环境系列卫星. 针对微波载荷高精度、高稳定度冷空观测任务需求,提出一种冷空定标技术,通过考虑起点和终点角速度的分段正弦轨迹规划方法可精准完成姿态机动轨迹规划,避免姿态机动超调,提升姿态机动稳定性. 结合卫星在轨运行特点,针对载荷展开、数据安全及能源安全开展了安全性设计,保障卫星长期稳态运行. 针对传统卫星控制分系统软件定制化程度高、研制周期长的问题,牵引了模块化、组件化、可复用的通用控制系统应用软件的设计,显著提升软件研制效率与质量可靠性. 针对专用测试设备硬件架构复杂、造价高、复用性差的问题,提出数字化通用验证技术,通过 “硬件通用化 + 软件可配置” 的测试设计,满足快速交付、降本增效的工程要求. 在轨飞行结果表明,上述设计可充分保障卫星快速交付及在轨长期安全、稳定、高效运行,成果已推广应用于多颗卫星.

     

    Abstract: Sea Surface Salinity Satellite is China’s first Satellitein the marine dynamic environment series dedicated to observing ocean salinity.Aiming at the requirements of high-precision and high-stability cold-space observation for microwave payloads, this paper proposes a cold-space calibration technology. By adopting a piecewise sinusoidal trajectory planning method considering the angular velocities at the start and end points, the attitude maneuver trajectory can be accurately planned, avoiding attitude maneuver overshoot and improving the stability of attitude maneuver. Combined with the on-orbit operation characteristics of the satellite, safety designs are carried out for payload deployment, floating-point calculation anomalies and energy security to ensure the long-term stable operation of the satellite. To address the problems of high customization, long development cycle of traditional satellite control subsystem software, a modular, component-based and reusable general application software is designed, which significantly improves the efficiency and quality reliability of software development. Aiming at the problems of complex hardware architecture, high cost and poor reusability of special test equipment, a digital general verification technology is proposed. Through the test design of "generalized hardware + configurable software", the engineering requirements of rapid delivery, cost reduction and efficiency improvement are met. The on-orbit flight results show that the above designs can fully guarantee the rapid delivery and long-term safe, stable and efficient on-orbit operation of the satellite, and have the value of cross-model promotion and application.

     

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