An Analysis of the Limit-Cycle and Structural-Resonance Characteristics of the X-15 Stability Augmentation System. Technical Report NASA Technical Note TN D-4287, Research Engineering, NASA Dryden Flight Research Center

Taylor Jr., Lawrence W. and Smith, John W. (1967) An Analysis of the Limit-Cycle and Structural-Resonance Characteristics of the X-15 Stability Augmentation System. Technical Report NASA Technical Note TN D-4287, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

Limit cycle and control surface resonance characteristics of X-15 stability augmentation system.

EPrint Type:	Other
Keywords:	Feedback control, Flight test vehicles, Resonant vibration, Stabilization, X-15 aircraft
Subjects:	(01 - 09) Aeronautics: (05) Aircraft Design, Testing And Performance Aircraft/Project: X-15
ID Code:	854
Deposited On:	12 April 2006
Additional Information:	51 pages.