Guidance, Navigation, and Control Conference and Exhibit · 1998 · 137 citations · 6 references
EngineeringAerospace EngineeringSystems EngineeringFault ToleranceFault-tolerant ComputingFault-tolerant SystemsAdaptive ControlAircraft ControlAugmentation SystemsFault DetectionFault-tolerant ControlNeural Control SystemsAdaptive Flight ControlChannelsControl AugmentationFault Tolerance ArchitectureFault Tolerance PerformanceFault-tolerant LandingFault-tolerant Nonlinear ControlTiltrotor Configuration
Anthony J. Calise Fellow AIAA Professor Georgia Institute of Technology Atlanta, GA This work is an extension of previous research at Georgia Tech. It demonstrates the fault-tolerance capabilities of a non-linear adaptive controller architecture. The XV-15 tiltrotor in landing configuration is used for demonstration. The failures considered affect longitudinal and lateral channels. Augmentation is provided successfully in all channels.
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