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THE METHOD OF THE USER-ORIENTED AGILE IMAGING SATELLITE DYNAMIC AUTONOMOUS MISSION SCHEDULING

机译:用户导向的敏捷成像卫星动态自主任务调度方法

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Directly to orient terrestrial users is an important application direction of earth observation satellites in the future. Through the terminal equipment on the ground, users upload the observed target information in real time. With the onboard computer, in allusion to the actual capacity for satellite, the in-orbit dynamic autonomous mission scheduling for multi-user and multi-objective is completed, and the imaging data is downloaded. In the article, with designing the user ID code uploaded by the terminal equipment on the ground, satellites could identify the priority of ground users, target properties, imaging requirements, timeliness information and the required ground station. Considering the attitude maneuver capability constraint, solar elevation angle constraint, mission timeliness constraint and minimum time interval constraint between two observed targets, the constraint satisfaction model of the uscr-oricntcd agile imaging satellite mission scheduling is established. For the in orbit computing power of satellites, dynamic heuristic rules that could achieve inserting new tasks in real time is designed. With the model and rules, satellites could autonomously complete orbit recursive, calculation of imaging integration time and drift angle compensation. Then, by autonomously generate the attitude guidance law and mission instruction sequence with the same model and rules, satellites autonomously achieve the mission scheduling, imaging and the data download. Finally, based on the simulation, the practicality of this model and algorithm is verified. With the result of our works, the foundation for the future user-oriented agile imaging satellite in-orbit dynamic autonomous mission scheduling is laid.
机译:直接面向地面用户是未来地球观测卫星的重要应用方向。用户通过地面上的终端设备,实时上传观察到的目标信息。利用车载计算机,根据卫星的实际容量,完成了针对多用户和多目标的在轨动态自主任务调度,并下载了成像数据。在本文中,通过设计终端设备在地面上载的用户ID代码,卫星可以识别地面用户的优先级,目标属性,成像要求,及时性信息和所需的地面站。考虑姿态机动能力约束,太阳仰角约束,任务时效性约束和两个观测目标之间的最小时间间隔约束,建立了实用的敏捷成像卫星任务调度约束满足模型。为了卫星的在轨计算能力,设计了可以实现实时插入新任务的动态启发式规则。利用该模型和规则,卫星可以自主完成轨道递归,成像积分时间的计算和漂移角补偿。然后,通过自主生成具有相同模型和规则的姿态制导律和任务指令序列,卫星自主实现任务调度,成像和数据下载。最后,基于仿真,验证了该模型和算法的实用性。通过我们的工作,为未来面向用户的敏捷成像卫星在轨动态自主任务调度奠定了基础。

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