Effect of model error on sensor placement for on-orbit modal identification of large space structures
- 1 March 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (2) , 334-341
- https://doi.org/10.2514/3.20841
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Sensor placement in structural controlJournal of Guidance, Control, and Dynamics, 1990
- Sensor and actuator selection for large space structure controlJournal of Guidance, Control, and Dynamics, 1990
- Test-analysis correlation of the Space Shuttle solid rocket motor center segmentJournal of Spacecraft and Rockets, 1989
- Optimum approximation for residual stiffness in linear system identificationAIAA Journal, 1988
- Perturbation bounds for robust stability in linear state space modelsInternational Journal of Control, 1985
- An eigensystem realization algorithm for modal parameter identification and model reductionJournal of Guidance, Control, and Dynamics, 1985
- Controllability and Observability of Linear Matrix-Second-Order SystemsJournal of Applied Mechanics, 1980
- Optimum experimental design for identification of distributed parameter systemsInternational Journal of Control, 1980
- A Methodology for Optimal Sensor Locations for Identification of Dynamic SystemsJournal of Applied Mechanics, 1978
- Observability and optimal measurement location in linear distributed parameter systems†International Journal of Control, 1973