In-Flight Suppression of an Unstable F/A-18 Structural Mode Using the Space Launch System Adaptive Augmenting Control System

NASA's Space Launch System (SLS) Flight Control System (FCS) includes an Adaptive Augmenting Control (AAC) component which employs a multiplicative gain update law to enhance the performance and robustness of the baseline control system for extreme off-nominal scenarios. The SLS FCS algorithm i...

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Hauptverfasser:	VanZwieten, Tannen S., Gilligan, Eric T., Wall, John H., Miller, Christopher J., Hanson, Curtis E., Orr, Jeb S.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aircraft Stability And Control Structural Mechanics
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