The feasibility of using piezoelectric ceramics as both sensors and actuators for vibration suppression in a lightweight, flimsy structure was demonstrated. Multimode control was achieved using one sensor and actuator pair. The Positive Position Feedback control strategy requires only knowledge of the natural frequencies of the structure. Implementation of the Positive Position Feedback used only strain measurements to achieve damping, no velocities, or acceleration are needed. All spillover is stabilizing for sufficient small gains
The purpose is to summarize a Phase 1 SBIR project performed for the NASA/Langley Computational Stru...
The focus is in the development of more accurate and efficient advanced methods for solution of sing...
The viewgraphs and discussion of the potential benefits and technology development requirements of s...
The progress and results are summarized for mission/system requirements database; mission analysis; ...
The High Speed Civil Transport (HSCT) mission perspective is given, along with the systems studies g...
An annual report that summarizes the work done on Grant No. NAG2-542 is presented. There are four ar...
This design study--the third in the space architecture series--focused on the requirements of an ear...
A miniaturized Cassegrainian concentrator (MCC) solar array concept is being developed with the obje...
The Timed Doppler Interferometer (TIDI) will accurately and precisely determine the global vector ML...
This is the eleventh in a series of evaluated sets of rate constants and photochemical cross section...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
The NASA budget request has been restructured in FY 1995 into four appropriations: human space fligh...
This study was undertaken to determine the velocity of fragments generated by the range safety destr...
The use of copper tubular thrust chambers is particularly important in high performance expander cyc...
Linear and angular vibration measurements for V/STOL aircraft, and strapdown inertial guidance syste...
The purpose is to summarize a Phase 1 SBIR project performed for the NASA/Langley Computational Stru...
The focus is in the development of more accurate and efficient advanced methods for solution of sing...
The viewgraphs and discussion of the potential benefits and technology development requirements of s...
The progress and results are summarized for mission/system requirements database; mission analysis; ...
The High Speed Civil Transport (HSCT) mission perspective is given, along with the systems studies g...
An annual report that summarizes the work done on Grant No. NAG2-542 is presented. There are four ar...
This design study--the third in the space architecture series--focused on the requirements of an ear...
A miniaturized Cassegrainian concentrator (MCC) solar array concept is being developed with the obje...
The Timed Doppler Interferometer (TIDI) will accurately and precisely determine the global vector ML...
This is the eleventh in a series of evaluated sets of rate constants and photochemical cross section...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
The NASA budget request has been restructured in FY 1995 into four appropriations: human space fligh...
This study was undertaken to determine the velocity of fragments generated by the range safety destr...
The use of copper tubular thrust chambers is particularly important in high performance expander cyc...
Linear and angular vibration measurements for V/STOL aircraft, and strapdown inertial guidance syste...
The purpose is to summarize a Phase 1 SBIR project performed for the NASA/Langley Computational Stru...
The focus is in the development of more accurate and efficient advanced methods for solution of sing...
The viewgraphs and discussion of the potential benefits and technology development requirements of s...