Utility of Concurrent Bandwidth Feedback in Training Aircraft Flight Tasks

In-Trim Flight Investigations of a Conceptual Fluidic Thrust-Vectored Unmanned Tail-Sitter Aircraft

The feasibility of using a stand alone Fluidic Thrust-Vectoring (FTV) system for the purpose of longitudinal trim of an unmanned aerial vehicle is the focus of the research presented in this paper. Since the fluidic thrust vectoring requires high pressure secondary air to deflect the engine exhaust gases, this research also provides an analytical toolset for preliminary sizing of a suitable sec...

calculation of aircraft aerodynamic loads during operational flight

in this research, the calculation method of aerodynamic loads on an airplane in all flight situations is presented. in order to find an calculation equation for aerodynamic loads on an airplane in all flight conditions, the f-5 aircraft is selected as a prototype is divided into one hundred small parts longitudinally. therefore, the numerical solutions are taken place in different conditions of...

Steady Aircraft Flight and Aircraft Performance

Vision-only Aircraft Flight Control

1 Graduate Research Assistant Email: [email protected] 2 Graduate Research Assistant Email: [email protected] 3 Lockheed Martin Assistant Professor of Avionics Integration Email: [email protected] Abstract Building aircraft with navigation and control systems that can complete flight tasks is complex, and often involves integrating information from multipl...

The Effect of Concurrent Bandwidth Feedback on Learning the Lane-Keeping Task in a Driving Simulator

OBJECTIVE The aim of this study was to investigate whether concurrent bandwidth feedback improves learning of the lane-keeping task in a driving simulator. BACKGROUND Previous research suggests that bandwidth feedback improves learning and that off-target feedback is superior to on-target feedback. This study aimed to extend these findings for the lane-keeping task. METHOD Participants with...