实验证明了一种采用闭环滤波器和控制器的方法来主动稳定卫星结构以抵抗热边界条件的随机扰动

IF 1.8 Q2 ENGINEERING, AEROSPACE

CEAS Space Journal Pub Date : 2023-07-15 DOI:10.1007/s12567-023-00514-y

F. Möller, T. Essig, S. Holzhauer, R. Förstner

引用次数: 0

摘要

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Experimental demonstration of a method to actively stabilize satellite structures against random perturbations of thermal boundary conditions using a closed-loop filter and controller approach

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来源期刊

CEAS Space Journal ENGINEERING, AEROSPACE-

CiteScore

3.90

自引率

7.10%

发文量

期刊介绍： The CEAS Space Journal has been created by the CEAS Space Branch to provide an appropriate platform for the excellent scientific publications submitted by scientists and engineers. Under the umbrella of CEAS, the German Aerospace Center (DLR) and the European Space Agency (ESA) support the Journal. The Journal is devoted to new developments and results in all areas of space-related science and technology, including important spin-off capabilities and applications as well as ground-based support systems and manufacturing advancements. Of interest are also (invited) in-depth reviews of the status of development in specific areas of relevance to space, and descriptions of the potential way forward. Typical disciplines of interest include mission design and space systems, satellite communications, aerothermodynamics (including physical fluid dynamics), environmental control and life support systems, materials, operations, space debris, optics, optoelectronics and photonics, guidance, navigation and control, mechanisms, propulsion, power, robotics, structures, testing and thermal issues and small satellites. The Journal publishes peer-reviewed original articles, (invited) reviews and short communications.