The handling qualities of the F-8 digital fly by wire airplane are evaluated by using the Cooper-Harper rating scale. The reasons for the ratings are given, as well as a short description of the flying tasks. It was concluded that the handling qualities of the airplane were good in most situations, although occasional ratings of unsatisfactory were given
The dynamic growth of general aviation as a mean of transport over medium distances means that peopl...
Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. Th...
A flight evaluation was conducted to determine the effect of engine throttle response characteristic...
The handling qualities of the F-8 digital fly-by-wire airplane are evaluated by using the Cooper-Har...
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
Flight test results of the F-8 digital fly-by-wire (DFBW) control system are presented and the impli...
The flying qualities of the CV-990 jet transport were evaluated over the normal operating flight env...
A flight-test program was conducted to determine the effect of advanced flight control systems and d...
The dynamical development of general aviation demands compilation of new aircraft control methods. T...
The introduction of fly-by-wire electronic flight control systems into transport aircraft has given...
An analytical study was conducted to evaluate the relative improvements in aircraft ride qualities t...
A redundant three-axis analog control system was designed and developed to back up a digital fly-by-...
NASA Dryden conducted a handling qualities experiment using a small displacement centerstick control...
The feasibility of using digital fly-by-wire systems to control aircraft was demonstrated by develop...
The data presented have no bearing on performance characteristics of airplane, which were considered...
The dynamic growth of general aviation as a mean of transport over medium distances means that peopl...
Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. Th...
A flight evaluation was conducted to determine the effect of engine throttle response characteristic...
The handling qualities of the F-8 digital fly-by-wire airplane are evaluated by using the Cooper-Har...
To assess the feasibility of a digital fly by wire system, the mechanical flight control system of a...
Flight test results of the F-8 digital fly-by-wire (DFBW) control system are presented and the impli...
The flying qualities of the CV-990 jet transport were evaluated over the normal operating flight env...
A flight-test program was conducted to determine the effect of advanced flight control systems and d...
The dynamical development of general aviation demands compilation of new aircraft control methods. T...
The introduction of fly-by-wire electronic flight control systems into transport aircraft has given...
An analytical study was conducted to evaluate the relative improvements in aircraft ride qualities t...
A redundant three-axis analog control system was designed and developed to back up a digital fly-by-...
NASA Dryden conducted a handling qualities experiment using a small displacement centerstick control...
The feasibility of using digital fly-by-wire systems to control aircraft was demonstrated by develop...
The data presented have no bearing on performance characteristics of airplane, which were considered...
The dynamic growth of general aviation as a mean of transport over medium distances means that peopl...
Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. Th...
A flight evaluation was conducted to determine the effect of engine throttle response characteristic...