Add to ORKGA study is made of the longitudinal response of a STOL airplane equipped with a vanecontrolled gust-alleviation system. Effects of various combinations of design parameters on the responses to horizontal and vertical gusts and to elevator inputs are presented. Almost complete gust alleviation may be obtained with this system when the center of gravity of the STOL airplane is at rearward locations, but pitch stability augmentation is required for satisfactory control characteristics
Analog computed time histories and altitude-ground track plots of swept wing transport aircraft long...
An airplane (light transport type) is assumed to be in level flight (no pitching) through atmospheri...
An analytical study was made of an optimal gust alleviation system that employs a vertical gust sens...
An analytical study has shown that a gust alleviation system for a STOL airplane in a cruise conditi...
The results of an analytical study of a system using stability derivatives determined in static wind...
A light airplane equipped with an automatic control system which drives large wing flaps and the sta...
Control laws were developed to investigate methods of alleviating the response of a STOL transport t...
A brief review is presented of the basic methods of gust alleviation. Some results obtained in fligh...
Results are given of an analysis of wing and horizontal-tail spar strains measured on a twin-engine ...
A passive aeromechanical gust alleviation system was examined for application to a Cessna 172. The s...
A designed control motion scheme to improve passenger comfort in general aviation aircraft by reduci...
A gust alleviation system for aircraft flying in turbulent air was analyzed. A vane sensor (with noi...
A designed control motion scheme to improve passenger comfort in general aviation aircraft by reduci...
Automatic control system design methods for gust and shear alleviation were studied. It is shown tha...
A simplified theory of aircraft vertical acceleration gust response based on a model including pitch...
Analog computed time histories and altitude-ground track plots of swept wing transport aircraft long...
An airplane (light transport type) is assumed to be in level flight (no pitching) through atmospheri...
An analytical study was made of an optimal gust alleviation system that employs a vertical gust sens...
An analytical study has shown that a gust alleviation system for a STOL airplane in a cruise conditi...
The results of an analytical study of a system using stability derivatives determined in static wind...
A light airplane equipped with an automatic control system which drives large wing flaps and the sta...
Control laws were developed to investigate methods of alleviating the response of a STOL transport t...
A brief review is presented of the basic methods of gust alleviation. Some results obtained in fligh...
Results are given of an analysis of wing and horizontal-tail spar strains measured on a twin-engine ...
A passive aeromechanical gust alleviation system was examined for application to a Cessna 172. The s...
A designed control motion scheme to improve passenger comfort in general aviation aircraft by reduci...
A gust alleviation system for aircraft flying in turbulent air was analyzed. A vane sensor (with noi...
A designed control motion scheme to improve passenger comfort in general aviation aircraft by reduci...
Automatic control system design methods for gust and shear alleviation were studied. It is shown tha...
A simplified theory of aircraft vertical acceleration gust response based on a model including pitch...
Analog computed time histories and altitude-ground track plots of swept wing transport aircraft long...
An airplane (light transport type) is assumed to be in level flight (no pitching) through atmospheri...
An analytical study was made of an optimal gust alleviation system that employs a vertical gust sens...