Published 2000
by National Aeronautics and Space Administration, Dryden Flight Research Center, Available from NASA Center for AeroSpace Information (CASI) in Edwards, Calif, Hanover, MD .
Written in English
Edition Notes
| Statement | John F. Carter and P. C. Stoliker. |
| Series | NASA/TM -- 2001-209024., NASA technical memorandum -- 209024. |
| Contributions | Stoliker, P. C., NASA Dryden Flight Research Center. |
| The Physical Object | |
|---|---|
| Format | Microform |
| Pagination | 1 v. |
| ID Numbers | |
| Open Library | OL16036968M |
NASA Dryden conducted a handling qualities experiment using a small displacement centerstick controller that Saab-Scania developed for the JAS 39 Gripen aircraft. The centerstick, or ministick, was mounted in the rear cockpit of an F/A aircraft. Flying Quality Analysis of a JAS 39 Gripen Ministick Controller in an F/A Aircraft John F. Carter NASA Dryden conducted a handling qualities experiment using a small displacement centerstick controller that Saab-Scania developed for the JAS 39 Gripen aircraft. 21st Century Collection of NASA and NACA Dryden Technical Reports: X-Plane, SR, Space Shuttle, Hypersonic Research, Fighter Planes (Two CD-ROM Set) [News, World Spaceflight] on *FREE* shipping on qualifying offers. 21st Century Collection of NASA and NACA Dryden Technical Reports: X-Plane, SR, Space Shuttle, Hypersonic Price: $ Analysis of control and guidance of rolling missiles with a single plane of control fins Flying quality analysis of a JAS 39 Gripen ministick controller in an F/A aircraft. John Carter and; P. Stoliker; No Access Implementation and testing of LPV controllers for the NASA F/A Systems Research Aircraft. Joseph Mueller and; Gary.
An Overview of Flight Test Results for a Formation Flight Autopilot. Flying Quality Analysis of a JAS 39 Gripen Ministick Controller in an F/A Aircraft. Article. Flying Quality Analysis Of A Jas 39 Gripen Ministick Controller In An F A 18 Aircraft Author: John F. Carter ISBN: NASA Vibro-Acoustic FE Analyses of the Saab Aircraft. NASA Technical Reports Server (NTRS) Green, Inge S. A finite element model of the Saab fuselage structure and interior cavity has been created in order to compute the noise level in the passenger cabin due to propeller noise. Areas covered in viewgraph format include the.
