The spacecraft autonomous control system is compared with the traditional spacecraft control system.
对自主运行和传统测控方式进行了比较。
Hence spacecraft control, state estimation systems are affected by the variations of the spacecraft's inertia parameters.
因而航天器的控制系统、状态估计系统将会受到航天器惯性参数变化的影响。
According to the requirements of modern spacecraft control, this paper presents a hierarchical intelligent adaptive control system based on the description of plant feature model knowledge.
针对现代航天器对控制任务的需求特点,基于航天器对象特征模型知识描述,提出了具有多层结构的智能自适应控制系统概念。
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