月球背面探测任务多目标协同控制模式设计

月球背面探测需要中继卫星提供中继通信支持,实现地面测控网对月面探测器的控制。为解决月球背面探测任务过程中和环月探测卫星等多个航天器目标的相互控制及其与地面测控网之间的复杂协同控制问题,提出了协同控制关联目标描述方法,明确了控制目标和上行路由的概念和确定原则、上行路由测控网资源分配原则,设计了基于时间窗口的中继测控资源分配方法、多目标协同控制的标称计划模式、遥操作规划模式和上行控制模式。经过"嫦娥4号"天地大回路无线联试和"鹊桥"中继卫星在轨飞行证明,设计是合理可行的。     

一种快速响应型小卫星的自主任务规划设计与应用

浦江一号卫星是由上海航天技术研究院研制的一颗快速响应型小卫星,于2015年9月成功发射,卫星质量347 kg,运行在高度481 km的太阳同步轨道。为高效、高精度识别定位地面大范围广泛而随机分布的电磁辐射目标,浦江一号卫星提出了基于单星电磁信号监测载荷与光学成像载荷综合应用的在轨自主任务规划方案。在轨应用表明:该设计解决了电磁信号监测与光学成像高效协同难题,实现了星上自主任务规划时间快于0.10 s,引导指向精度优于0.10°,单次任务连续引导目标数量多于10个,为后续多手段遥感卫星的综合应用及在轨自主任务规划设计提供借鉴。     

模块化开放式航空电子系统架构标准研究

国外对开放式系统架构（OSA）概念的探索至今已有40 多年。美国国防部模块化开放式系统方法 （MOSA）正是建立在OSA 概念之上，综合了采办和工程方法，来实现低成本、优化和快速能力升级的武器 系统灵活开发。本文将集中讨论MOSA 构建方法及其开放式架构的最佳实践，包括开放式任务系统、未来机 载能力环境和传感器开放式系统架构。最后，本文讨论了MOSA 在开放式架构上开展的工作及其挑战，以期 对我国在航空电子OSA 标准研究和实践上有所裨益。     

Closed-form solution of attitude command generation for spin-to-spin maneuver

In recent earth observing missions, agile satellites enable various imaging modes beyond the traditional along-track strip imaging. However, it requires maneuvering with boundary conditions of considerable angular velocity, i.e., spin-to-spin maneuvering. This paper proposes an attitude command generation method for spin-to-spin maneuvering that can provide feedforward commands for the attitude control loop. A general solution for arbitrary flight time is provided which steers a satellite to the given final attitude and angular velocity at the prescribed time. In addition, an alternative method is proposed that further improves the maneuvering speed, which is applicable to small-angle maneuvering cases. The proposed solutions are both closed-form which are more intuitive and easier to comprehend than numerical solutions. It also has a great advantage in computational efficiency, which could enable its use on-board in real time. Numerical examples demonstrate the performance of the proposed methods in a single maneuvering case as well as in a consecutive maneuvering case integrated with a realistic earth observing scenario.     

Solar ring mission: Building a panorama of the Sun and inner-heliosphere

Solar Ring (SOR) is a proposed space science mission to monitor and study the Sun and inner heliosphere from a full 360° perspective in the ecliptic plane. It will deploy-three 120°-separated spacecraft on the 1-AU orbit. The first spacecraft, S1, locates 30° upstream of the Earth, the second, S2, 90° downstream, and the third, S3, completes the configuration. This design with necessary science instruments, e.g., the Doppler-velocity and vector magnetic field imager, wide-angle coronagraph, and in-situ instruments, will allow us to establish many unprecedented capabilities: (1) provide simultaneous Doppler-velocity observations of the whole solar surface to understand the deep interior, (2) provide vector magnetograms of the whole photosphere — the inner boundary of the solar atmosphere and heliosphere, (3) provide the information of the whole lifetime evolution of solar featured structures, and (4) provide the whole view of solar transients and space weather in the inner heliosphere. With these capabilities, Solar Ring mission aims to address outstanding questions about the origin of solar cycle, the origin of solar eruptions and the origin of extreme space weather events. The successful accomplishment of the mission will construct a panorama of the Sun and inner-heliosphere, and therefore advance our understanding of the star and the space environment that holds our life.     

遥感卫星多路数据传输系统同频共用方法

为节省频率资源，遥感卫星通常采用扩频体制实现多路数据的同频共用传输，针对通道间容易引起相互干扰的问题进行了研究，通过改进码分多址干扰估算模型，对采用平衡Gold码序列扩频系统抗干扰容限上界进行预测。在满足国际电信联盟（ITU）对卫星辐射功率通量密度约束条件下，提出了一种基于直接序列扩频体制的两路业务数据同频共用传输方法。仿真结果表明：当载波频率2GHz左右，两路辐射源的EIRP之差不大于8～15dBw时可以实现同频共用传输；如对信号扩频带宽进行差异化处理，则其相互兼容性还可进一步提高。     

Autonomous mission reconstruction during the ascending flight of launch vehicles under typical propulsion system failures

In recent years, Chinese Long March(LM) launchers have experienced several launch failures, most of which occurred in their propulsion systems, and this paper studies Autonomous Mission Reconstruction(AMRC) technology to alleviate losses due to these failures. The status of the techniques related to AMRC, including trajectory and mission planning, guidance methods,and fault tolerant technologies, are reviewed, and their features are compared, which reflect the challenges faced by AMRC technology...