An analytical study has shown that, with proper selection of feedback gains, an automatic control system can reduce excursions in altitude of a jet transport flying in turbulence without increasing structural loads. The control system uses feedback of attitude-angle and pitch-rate signals to the elevator and uses feedback of altitude and altitude-rate signals to the throttle
A static stability augmentation system (SSAS) with angle-of-attack, pitch-rate, and forward-speed fe...
A flight-test program was conducted to determine the effect of advanced flight control systems and d...
In the aviation industry, aircraft manufactures are constantly striving to fully understand the esse...
An analytical study has been made to assess the loads developed on the horizontal tail of an autopil...
An analytical study has shown that a gust alleviation system for a STOL airplane in a cruise conditi...
A simplified theory of aircraft vertical acceleration gust response based on a model including pitch...
A light airplane equipped with an automatic control system which drives large wing flaps and the sta...
A study is made of the longitudinal response of a STOL airplane equipped with a vanecontrolled gust-...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Bi...
Cover titleJanuary 1988Also issued as an M.S. thesis, Massachusetts Institute of Technology, Dept. o...
Longitudinal performance and control utilization data are compared for several different automatic a...
An analytical and experimental investigation of possible contributing factors in jet aircraft turbul...
Atmospheric turbulence effects on stability and response characteristics of subsonic jet transport a...
An analytical study was conducted to evaluate the relative improvements in aircraft ride qualities t...
Aircraft specifically designed for short take-off and landing (STOL) operations are particularly sen...
A static stability augmentation system (SSAS) with angle-of-attack, pitch-rate, and forward-speed fe...
A flight-test program was conducted to determine the effect of advanced flight control systems and d...
In the aviation industry, aircraft manufactures are constantly striving to fully understand the esse...
An analytical study has been made to assess the loads developed on the horizontal tail of an autopil...
An analytical study has shown that a gust alleviation system for a STOL airplane in a cruise conditi...
A simplified theory of aircraft vertical acceleration gust response based on a model including pitch...
A light airplane equipped with an automatic control system which drives large wing flaps and the sta...
A study is made of the longitudinal response of a STOL airplane equipped with a vanecontrolled gust-...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.Bi...
Cover titleJanuary 1988Also issued as an M.S. thesis, Massachusetts Institute of Technology, Dept. o...
Longitudinal performance and control utilization data are compared for several different automatic a...
An analytical and experimental investigation of possible contributing factors in jet aircraft turbul...
Atmospheric turbulence effects on stability and response characteristics of subsonic jet transport a...
An analytical study was conducted to evaluate the relative improvements in aircraft ride qualities t...
Aircraft specifically designed for short take-off and landing (STOL) operations are particularly sen...
A static stability augmentation system (SSAS) with angle-of-attack, pitch-rate, and forward-speed fe...
A flight-test program was conducted to determine the effect of advanced flight control systems and d...
In the aviation industry, aircraft manufactures are constantly striving to fully understand the esse...