Parameter Identification of Large Spacecraft Systems, Based on the Frequency Characteristics of the Hankel Operator
Journal : M.S. Thesis Number: CSHCN MS 92-3
December 31, 1991
The identification of the structural modes and damping factors of a spacecraft in orbit is accomplished. A systems approach was used to analyze the experiment and present identification techniques utilizing the frequency characteristics of the Hankel operator. Frequency domain error bounds and time domain error bounds are considered.