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Sensor/actuator placement for flexible space structuresA new approach for the placement of sensors and actuators in the active control of flexible space structures is developed. The approach converts the discrete nature of the sensor and actuator positioning problem to a nonlinear programming optimization through approximation of the control forces and output measurements by spatially continuous functions. The locations of the sensors and actuators are optimized in order to move the transmission zeros of the system farther to the left of the imaginary axis. The criterion for sensor/actuator placement can be quite useful for optimal regulation and tracking problems, as well as for low-authority controller designs. Two performance metrics are considered for the optimization and are applied to the sensor/actuator positioning of a large-order flexible space structure.
Document ID
19910045544
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Maghami, P. G.
(NASA Langley Research Center Hampton, VA, United States)
Joshi, S. M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91A30167
Distribution Limits
Public
Copyright
Other

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