Adaptive structures and mechatronic components for vibration and shape control of satellite precision payloads

H. Baier, M. Müller

Research output: Contribution to conferencePaperpeer-review

1 Scopus citations

Abstract

Smart materials and actuators for in-orbit jitter and shape control for precision instruments are discussed together with effects of very low temperatures and eventual nonlinearities. Simulation and lab model demonstration results together with different types of actuators are given for solar array and precision optical bank active vibration attenuation as well as for reflector shape control. The latter calls for circumferentially and radially arranged actuators.

Original languageEnglish
Pages1772-1778
Number of pages7
StatePublished - 2003
Event54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law - Bremen, Germany
Duration: 29 Sep 20033 Oct 2003

Conference

Conference54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law
Country/TerritoryGermany
CityBremen
Period29/09/033/10/03

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