An analog computer study of several stability augmentation schemes designed to alleviate roll-induced instability
Description: From Introduction: "The purpose of the present study is to investigate these suggested methods for reducing the undesirable pitching and yawing motions of an airplane during roll maneuvers. The airplane characteristics used in this study were those of the F-100A airplane having the original small vertical tail as shown in figure 1."
Date: February 19, 1957
Creator: Creer, Brent Y.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department