Flight Determined Subsonic Longitudinal Stability And Control Derivatives Of The F 18 High Angle Of Attack Research Vehicle Harv With Thrust Vectoring PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Flight Determined Subsonic Longitudinal Stability And Control Derivatives Of The F 18 High Angle Of Attack Research Vehicle Harv With Thrust Vectoring PDF full book. Access full book title Flight Determined Subsonic Longitudinal Stability And Control Derivatives Of The F 18 High Angle Of Attack Research Vehicle Harv With Thrust Vectoring.
Author | : Kenneth W. Iliff |
Publisher | : |
Total Pages | : 74 |
Release | : 1997 |
Genre | : Aerodynamics |
ISBN | : |
Download Flight-Determined Subsonic Longitudinal Stability and Control Derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with Thrust Vectoring Book in PDF, ePub and Kindle
Author | : Kenneth W. Iliff |
Publisher | : |
Total Pages | : 92 |
Release | : 1999 |
Genre | : Aerodynamics |
ISBN | : |
Download Flight-Determined, Subsonic, Lateral-Directional Stability and Control Derivatives of the Thrust-Vectoring F-18 High Angle of Attack Research Vehicle (HARV), and Comparisons to the Basic F-18 and Predicted Derivatives Book in PDF, ePub and Kindle
Author | : Robert G. Ferguson |
Publisher | : |
Total Pages | : 312 |
Release | : 2013 |
Genre | : Aeronautics |
ISBN | : |
Download NASA's First A Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 658 |
Release | : 2000 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, ePub and Kindle
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 124 |
Release | : 2018-07-17 |
Genre | : |
ISBN | : 9781723022715 |
Download Determination of the Stability and Control Derivatives of the NASA F/A-18 Harv Using Flight Data Book in PDF, ePub and Kindle
This report documents the research conducted for the NASA-Ames Cooperative Agreement No. NCC 2-759 with West Virginia University. A complete set of the stability and control derivatives for varying angles of attack from 10 deg to 60 deg were estimated from flight data of the NASA F/A-18 HARV. The data were analyzed with the use of the pEst software which implements the output-error method of parameter estimation. Discussions of the aircraft equations of motion, parameter estimation process, design of flight test maneuvers, and formulation of the mathematical model are presented. The added effects of the thrust vectoring and single surface excitation systems are also addressed. The results of the longitudinal and lateral directional derivative estimates at varying angles of attack are presented and compared to results from previous analyses. The results indicate a significant improvement due to the independent control surface deflections induced by the single surface excitation system, and at the same time, a need for additional flight data especially at higher angles of attack. Napolitano, Marcello R. and Spagnuolo, Joelle M. Unspecified Center AIRCRAFT CONTROL; AIRCRAFT STABILITY; ANGLE OF ATTACK; F-18 AIRCRAFT; FLIGHT TESTS; LATERAL STABILITY; LONGITUDINAL STABILITY; MAXIMUM LIKELIHOOD ESTIMATES; PARAMETER IDENTIFICATION; AIRCRAFT MANEUVERS; CONTROL SURFACES; EQUATIONS OF MOTION; MATHEMATICAL MODELS; THRUST VECTOR CONTROL...
Author | : |
Publisher | : |
Total Pages | : 30 |
Release | : 1991 |
Genre | : |
ISBN | : |
Download Research Flight-control System Development for the F-18 High Alpha Research Vehicle Book in PDF, ePub and Kindle
Author | : Kenneth W. Iliff |
Publisher | : |
Total Pages | : 40 |
Release | : 1976 |
Genre | : Airplanes |
ISBN | : |
Download Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8 Scale F-15 Airplane Model Obtained from Flight Test Book in PDF, ePub and Kindle
Author | : Eugene A. Morelli |
Publisher | : |
Total Pages | : 54 |
Release | : 1995 |
Genre | : |
ISBN | : |
Download The F-18 High Alpha Research Vehicle (HARV) Parameter Identification Flight Test Maneuvers for Optimal Input Design Validation and Lateral Control Book in PDF, ePub and Kindle
Flight tests maneuvers are specified for the F-18 Alpha Research Vehicle (HARV). The maneuvers were designed for open loop parameter identification purposes, specifically for optimal input design validation at 5 degrees angle of attack, identification of individual strake effectiveness at 40 and 50 degrees angle of attack, and study of lateral dynamics and lateral control effectiveness at 40 and 50 degrees angle of attack. Each maneuver is to be realized by applying square wave inputs to specific control effectors using the On-Board Excitation System (OBES). Maneuver descriptions and complete specifications of the time/amplitude points defining each input are included, along with plots of the input time histories.
Author | : |
Publisher | : |
Total Pages | : 18 |
Release | : 1990 |
Genre | : |
ISBN | : |
Download Validation of the F-18 High Alpha Research Vehicle Flight Control and Avionics Systems Modifications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 68 |
Release | : 1994 |
Genre | : |
ISBN | : |
Download High-Alpha Research Vehicle (HARV) Longitudinal Controller: Design, Analyses, and Simulation Resultss Book in PDF, ePub and Kindle