This paper summarizes work performed under a collaborative research effort between NASA and the German Aerospace Research Establishment (DLR, Deutsche Forschungsanstalt fuer Luft- und Raumfahrt). The objective is to develop and demonstrate advanced technology for system identification of future large space structures. Recent experiences using the Eigensystem Realization Algorithm (ERA) for modal identification of Mini-Mast are reported. Mini-Mast is a 20-meter long deployable space truss used for structural dynamics and active vibration-control research at the NASA Langley Research Center. Due to nonlinearities and numerous local modes, modal idenfification of Mini-Mast proved to be surprisingly difficult. Methods available with ERA for...
In this paper an operational technique for the vibrating condition identification, based on the use ...
A determinação de características dinâmicas de estruturas aeronáuticas é um assunto extremamente imp...
Following the mechanical verification logic of spacecraft structures, a comprehensive programme of s...
Work performed under a collaborative research effort between NASA and the German Aerospace Research ...
This paper summarizes work performed under a collaborative research effort between the National Aero...
This paper summarizes work performed under a collaborative research effort between NASA and the Germ...
This paper summarizes modal identification results obtained using an autonomous version of the Eigen...
This paper discusses work performed under a collaborative research agreement between NASA and DLR in...
Future large space structures such as Space Station Freedom cannot be tested as a total structure on...
The Mini-Mast is a 20 meter long 3-dimensional, deployable/retractable truss structure designed to i...
With complex structures, comparison of independently derived sets of experimental modal parameters i...
It is beneficial to use a distributed parameter model for large space structures because the approac...
The modal identification of large aerospace structures like aircraft prototypes or satellites requir...
Vibrations represent one of the most important topics of the engineering design relevant to flexible...
Recent laboratory results using a refined phase resonance method and the eigensystem realization alg...
In this paper an operational technique for the vibrating condition identification, based on the use ...
A determinação de características dinâmicas de estruturas aeronáuticas é um assunto extremamente imp...
Following the mechanical verification logic of spacecraft structures, a comprehensive programme of s...
Work performed under a collaborative research effort between NASA and the German Aerospace Research ...
This paper summarizes work performed under a collaborative research effort between the National Aero...
This paper summarizes work performed under a collaborative research effort between NASA and the Germ...
This paper summarizes modal identification results obtained using an autonomous version of the Eigen...
This paper discusses work performed under a collaborative research agreement between NASA and DLR in...
Future large space structures such as Space Station Freedom cannot be tested as a total structure on...
The Mini-Mast is a 20 meter long 3-dimensional, deployable/retractable truss structure designed to i...
With complex structures, comparison of independently derived sets of experimental modal parameters i...
It is beneficial to use a distributed parameter model for large space structures because the approac...
The modal identification of large aerospace structures like aircraft prototypes or satellites requir...
Vibrations represent one of the most important topics of the engineering design relevant to flexible...
Recent laboratory results using a refined phase resonance method and the eigensystem realization alg...
In this paper an operational technique for the vibrating condition identification, based on the use ...
A determinação de características dinâmicas de estruturas aeronáuticas é um assunto extremamente imp...
Following the mechanical verification logic of spacecraft structures, a comprehensive programme of s...