Abstract: No abstract available
Author: New NASA STI
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Abstract: No abstract available
Determining the Products of Inertia for Small Scale UAVs
Abstract: Moments of inertia and products of inertia often need to be determined for aircraft. As…
New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity
Abstract: This presentation is a conference companion and discusses a new flutter analysis technique using CFD…
SpaRibs Geometry Parameterization for Wings with Multiple Sections using Single Design
Abstract: The SpaRibs topology of an aircraft wing has a significant effect on its structural behavior…
Methods of Constructing a Blended Performance Function Suitable for Formation Flight
Abstract: This paper presents two methods for constructing an approximate performance function of a desired parameter…
Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression, Flight-Test Performance
Abstract: The problem of control command and maneuver induced structural loads is an important aspect of…
Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression, Experiment Development
Abstract: The problem of control command and maneuver induced structural loads is an important aspect of…
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Abstract: One of the most severe forms of coupling between aeroelasticity and flight dynamics is an…
New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity
Abstract: A new time-domain approach for computing flutter speed is presented. Based on the time-history result…