This paper describes the design, analysis, and nonlinear simulation results (batch and piloted) for a longitudinal controller which is scheduled to be flight-tested on the High-Alpha Research Vehicle (HARV). The HARV is an F-18 airplane modified for and equipped with multi-axis thrust vectoring. The paper includes a description of the facilities, a detailed review of the feedback controller design, linear analysis results of the feedback controller, a description of the feed-forward controller design, nonlinear batch simulation results, and piloted simulation results. Batch simulation results include maximum pitch stick agility responses, angle of attack alpha captures, and alpha regulation for full lateral stick rolls at several alpha's. P...
This progress report presents the results of an investigation focused on parameter identification fo...
This report documents the research conducted for the NASA-Ames Cooperative Agreement No. NCC 2-759 w...
This paper highlights some of the results and issues associated with estimating models to evaluate c...
Flight test maneuvers are specified for the F-18 High Alpha Research Vehicle (HARV). The maneuvers w...
The subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Researc...
The 'f18harv' six degree-of-freedom nonlinear batch simulation used to support research in advanced ...
The design of nonlinear controllers has relied on the use of detailed aerodynamic and engine models ...
Flight test maneuvers are specified for the F-18 High Alpha Research Vehicle (HARV). The maneuvers w...
This report presents the results of analysis of cockpit lateral control feel-system studies. Variati...
Flight test maneuvers are specified for the F-18 High Alpha Research Vehicle (HARV). The maneuvers w...
The NASA F/A-18 High Alpha Research Vehicle (HARV) has been the flight test bed of a focused technol...
A methodology is described for the development of flight test trajectory control laws based on singu...
The purpose was to develop and apply new nonlinear system methodologies to the stability analysis an...
This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehic...
The NASA High-Angle-of Attack Research Vehicle (HARV), a modified F-18 aircraft, experienced handlin...
This progress report presents the results of an investigation focused on parameter identification fo...
This report documents the research conducted for the NASA-Ames Cooperative Agreement No. NCC 2-759 w...
This paper highlights some of the results and issues associated with estimating models to evaluate c...
Flight test maneuvers are specified for the F-18 High Alpha Research Vehicle (HARV). The maneuvers w...
The subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Researc...
The 'f18harv' six degree-of-freedom nonlinear batch simulation used to support research in advanced ...
The design of nonlinear controllers has relied on the use of detailed aerodynamic and engine models ...
Flight test maneuvers are specified for the F-18 High Alpha Research Vehicle (HARV). The maneuvers w...
This report presents the results of analysis of cockpit lateral control feel-system studies. Variati...
Flight test maneuvers are specified for the F-18 High Alpha Research Vehicle (HARV). The maneuvers w...
The NASA F/A-18 High Alpha Research Vehicle (HARV) has been the flight test bed of a focused technol...
A methodology is described for the development of flight test trajectory control laws based on singu...
The purpose was to develop and apply new nonlinear system methodologies to the stability analysis an...
This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehic...
The NASA High-Angle-of Attack Research Vehicle (HARV), a modified F-18 aircraft, experienced handlin...
This progress report presents the results of an investigation focused on parameter identification fo...
This report documents the research conducted for the NASA-Ames Cooperative Agreement No. NCC 2-759 w...
This paper highlights some of the results and issues associated with estimating models to evaluate c...