This paper describes a series of modal tests that were performed on a cantilevered truss structure. The goal of the tests was to assemble a large database of high quality modal test data for use in verification of proposed methods for on orbit model verification and damage detection in flexible truss structures. A description of the hardware is provided along with details of the experimental setup and procedures for 16 damage cases. Results from selected cases are presented and discussed. Differences between ground vibration testing and on orbit modal testing are also described
A spacecraft payload flown on a launch vehicle experiences dynamic loads. The dynamic loads are caus...
Vibration testing spaceflight hardware is a vital, but time consuming and expensive endeavor. Tradit...
The design, construction, and operation of a low-Earth orbit space station poses challenges for deve...
A three-dimensional scale model of a hexagonal boom truss of the then space station Freedom was buil...
Independent of the modal identification techniques employed for damage detection, use of measured mo...
The long lifetimes, delicate nature and stringent pointing requirements of large space structures su...
Locating damaged truss members in large space structures will involve a combination of sensing and d...
The damage location approach employs the control system capabilities for the structure to test the s...
The complexity and size of the next generation of spacecraft, along with the exceedingly high perfor...
This paper summarizes the experimental program, the modal test results, the extracted modal shapes a...
Spacecraft structures are subjected to severe environmental mechanical loads, especially during the ...
A large fixture was designed and constructed for modal vibration testing of International Space Stat...
On-orbit testing of a large space structure will be required to complete the certification of any ma...
The Space Station Structural Characterization Experiment (SSSCE) 1,2 is an early space flight experi...
The research focused on the development of a new method to identify damaged structural elements from...
A spacecraft payload flown on a launch vehicle experiences dynamic loads. The dynamic loads are caus...
Vibration testing spaceflight hardware is a vital, but time consuming and expensive endeavor. Tradit...
The design, construction, and operation of a low-Earth orbit space station poses challenges for deve...
A three-dimensional scale model of a hexagonal boom truss of the then space station Freedom was buil...
Independent of the modal identification techniques employed for damage detection, use of measured mo...
The long lifetimes, delicate nature and stringent pointing requirements of large space structures su...
Locating damaged truss members in large space structures will involve a combination of sensing and d...
The damage location approach employs the control system capabilities for the structure to test the s...
The complexity and size of the next generation of spacecraft, along with the exceedingly high perfor...
This paper summarizes the experimental program, the modal test results, the extracted modal shapes a...
Spacecraft structures are subjected to severe environmental mechanical loads, especially during the ...
A large fixture was designed and constructed for modal vibration testing of International Space Stat...
On-orbit testing of a large space structure will be required to complete the certification of any ma...
The Space Station Structural Characterization Experiment (SSSCE) 1,2 is an early space flight experi...
The research focused on the development of a new method to identify damaged structural elements from...
A spacecraft payload flown on a launch vehicle experiences dynamic loads. The dynamic loads are caus...
Vibration testing spaceflight hardware is a vital, but time consuming and expensive endeavor. Tradit...
The design, construction, and operation of a low-Earth orbit space station poses challenges for deve...