Parameter identification using experimental modal data is examined. The following approaches are discussed: (1) Direct - using actual sensor measurements to obtain parameters (e.g., ERA, ITD); and (2) Indirect - identifies parameters using measured modal data. In this work, only the natural frequencies are used to identify physical parameters
The Control of Flexible Structures II (CPFS) program is a complex and ambitious undertaking which ad...
The objective was to predict the inherent turbulence response characteristics of candidate wind shea...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
Viewgraphs on finite element model and identification procedure are presented. Topics covered includ...
The following pages describe the development of a nonlinear simulation, results for the Martian entr...
Integrated airframe/propulsion control system architecture is discussed. The main objectives of the ...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
POSIX is an evolving set of operating system interface standards, whose parts are in varying stages ...
A point mass, three-degree of freedom model is presented as a basic development tool for PC based si...
A computational procedure is described which can be used efficiently in identifying modeling errors ...
Several topics related to the assessment of fault-tolerant design principles for software are presen...
The elements of the test program for the space suit to be used on Space Station Freedom are noted in...
Information is given in viewgraph form on advanced flight software reconfiguration. Reconfiguration ...
Cold working holes for improved fatigue life of fastener holes are widely used on aircraft. This pap...
The design of turbomachinery blades requires the prevention of flutter for all operating conditions....
The Control of Flexible Structures II (CPFS) program is a complex and ambitious undertaking which ad...
The objective was to predict the inherent turbulence response characteristics of candidate wind shea...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...
Viewgraphs on finite element model and identification procedure are presented. Topics covered includ...
The following pages describe the development of a nonlinear simulation, results for the Martian entr...
Integrated airframe/propulsion control system architecture is discussed. The main objectives of the ...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
POSIX is an evolving set of operating system interface standards, whose parts are in varying stages ...
A point mass, three-degree of freedom model is presented as a basic development tool for PC based si...
A computational procedure is described which can be used efficiently in identifying modeling errors ...
Several topics related to the assessment of fault-tolerant design principles for software are presen...
The elements of the test program for the space suit to be used on Space Station Freedom are noted in...
Information is given in viewgraph form on advanced flight software reconfiguration. Reconfiguration ...
Cold working holes for improved fatigue life of fastener holes are widely used on aircraft. This pap...
The design of turbomachinery blades requires the prevention of flutter for all operating conditions....
The Control of Flexible Structures II (CPFS) program is a complex and ambitious undertaking which ad...
The objective was to predict the inherent turbulence response characteristics of candidate wind shea...
In Jan. 1991, the LaRc SSFO performed an assessment of the configuration characteristics of the prop...