The Photogrammetric Appendage Structural Dynamics Experiment was designed, developed, and flown to demonstrate and prove measurement of the structural vibration response of a Russian Space Station Mir solar array using photogrammetric methods. The experiment flew on the STS-74 Space Shuttle mission to Mir in November 1995 and obtained video imagery of solar array structural response to various excitation events. The video imagery has been digitized and triangulated to obtain response time history data at discrete points on the solar array. This data has been further processed using the Eigensystem Realization Algorithm modal identification technique to determine the natural vibration frequencies, damping, and mode shapes of the solar array....
sciences mission, analysis of data from the rst 370 days after launch was used to investigate in- ...
The Roll-Out Solar Array (ROSA) flight experiment was launched to the International Space Station (I...
In order to be cost-effective, space structures must be extremely light-weight, and subsequently, ve...
The Photogrammetric Appendage Structural Dynamics Experiment was designed, developed, and flown to d...
The Photogrammetric Appendage Structural Dynamics Experiment (PASDE) is an International Space Stati...
The Photogrammetric Appendage Structural Dynamics Experiment (PASDE) uses six video cameras in the S...
The Photogrammetric Appendage Structural Dynamics Experiment (PASDE) is a Hitchhiker payload schedul...
Vibrations represent one of the most important topics of the engineering design relevant to flexible...
Understanding the dynamic characteristics of solar arrays is important for satellite structural desi...
The Roll-Out Solar Array (ROSA) flight experiment was launched to the International Space Station (I...
This paper summarizes in-space structural validation plans for a proposed Space Shuttle-based flight...
Abstract: Video information about vibrations of elements of ISS structure allows to establ...
The purpose of the Solar Array Flight Dynamic Experiment (SAFDE) is to demonstrate the feasibility o...
Future large space structures such as Space Station Freedom cannot be tested as a total structure on...
Future large space structures such as Space Station Freedom cannot be tested as a total structure on...
sciences mission, analysis of data from the rst 370 days after launch was used to investigate in- ...
The Roll-Out Solar Array (ROSA) flight experiment was launched to the International Space Station (I...
In order to be cost-effective, space structures must be extremely light-weight, and subsequently, ve...
The Photogrammetric Appendage Structural Dynamics Experiment was designed, developed, and flown to d...
The Photogrammetric Appendage Structural Dynamics Experiment (PASDE) is an International Space Stati...
The Photogrammetric Appendage Structural Dynamics Experiment (PASDE) uses six video cameras in the S...
The Photogrammetric Appendage Structural Dynamics Experiment (PASDE) is a Hitchhiker payload schedul...
Vibrations represent one of the most important topics of the engineering design relevant to flexible...
Understanding the dynamic characteristics of solar arrays is important for satellite structural desi...
The Roll-Out Solar Array (ROSA) flight experiment was launched to the International Space Station (I...
This paper summarizes in-space structural validation plans for a proposed Space Shuttle-based flight...
Abstract: Video information about vibrations of elements of ISS structure allows to establ...
The purpose of the Solar Array Flight Dynamic Experiment (SAFDE) is to demonstrate the feasibility o...
Future large space structures such as Space Station Freedom cannot be tested as a total structure on...
Future large space structures such as Space Station Freedom cannot be tested as a total structure on...
sciences mission, analysis of data from the rst 370 days after launch was used to investigate in- ...
The Roll-Out Solar Array (ROSA) flight experiment was launched to the International Space Station (I...
In order to be cost-effective, space structures must be extremely light-weight, and subsequently, ve...