NASA NTRS · 19740003696
Analysis and testing of stability augmentation systems
Abstract
Testing and evaluation of stability augmentation systems for aircraft flight control were conducted. The flutter suppression system analysis of a scale supersonic transport wing model is described. Mechanization of the flutter suppression system is reported. The ride control synthesis for the B-52 aeroelastic model is discussed. Model analyses were conducted using equations of motion generated from generalized mass and stiffness data.
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Sevart, F. D., Patel, S. M., Wattman, W. J.. 1972-06-13. Analysis and testing of stability augmentation systems. https://ntrs.nasa.gov/citations/19740003696
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