Structural dynamics identification is a common, long-standing procedure performed on large aerospace structures in order to investigate their dynamic behavior. Usually, the experimental identification is accomplished by a set of single exciters placed at suitable structural points. An alternative to multiple point excitation is a driven-base test using a multi-axial shaker table
The modal identification of large aerospace structures like aircraft prototypes or satellites requir...
The vibration characteristics of aerospace structures are investigated in so-called ground vibration...
Modal parameter estimates of a structure, vibrating under actual loadings and operational conditions...
Dynamic qualification of spacecraft structures usually are performed on special vibration test facil...
This paper deals with the identification of effective masses and modal masses from base-driven tests...
A multi-axial shaking table is normally used for earthquake simulation and the dynamic qualification...
The multi-axis shaker is often used for the dynamic qualification of aerospace structures. The vibra...
Most of the commonly used modal testing methods are based on multiple point excitation. An alternat...
A structural model of a satellite has been employed for vibration tests on two multi-axis vibration ...
Most of the commonly used modal testing methods are based on multiple point excitation. The interfa...
This paper concentrates on the fundamentals of the structural vibration behaviour of a structure und...
Normal mode testing is commonly performed on large aerospace structures in order to identify their e...
The modal identification of a structure consists in providíng the parameters representing this speci...
A time domain identification method analysing forced vibrations is utisized for evaluation of a base...
Dynamic acceptance tests with the PPF/ENVISAT-1 Flight Model are planned to be performed in August 2...
The modal identification of large aerospace structures like aircraft prototypes or satellites requir...
The vibration characteristics of aerospace structures are investigated in so-called ground vibration...
Modal parameter estimates of a structure, vibrating under actual loadings and operational conditions...
Dynamic qualification of spacecraft structures usually are performed on special vibration test facil...
This paper deals with the identification of effective masses and modal masses from base-driven tests...
A multi-axial shaking table is normally used for earthquake simulation and the dynamic qualification...
The multi-axis shaker is often used for the dynamic qualification of aerospace structures. The vibra...
Most of the commonly used modal testing methods are based on multiple point excitation. An alternat...
A structural model of a satellite has been employed for vibration tests on two multi-axis vibration ...
Most of the commonly used modal testing methods are based on multiple point excitation. The interfa...
This paper concentrates on the fundamentals of the structural vibration behaviour of a structure und...
Normal mode testing is commonly performed on large aerospace structures in order to identify their e...
The modal identification of a structure consists in providíng the parameters representing this speci...
A time domain identification method analysing forced vibrations is utisized for evaluation of a base...
Dynamic acceptance tests with the PPF/ENVISAT-1 Flight Model are planned to be performed in August 2...
The modal identification of large aerospace structures like aircraft prototypes or satellites requir...
The vibration characteristics of aerospace structures are investigated in so-called ground vibration...
Modal parameter estimates of a structure, vibrating under actual loadings and operational conditions...