A flight control type system which provides a tactile readout to the hand of a pilot for directing elevator control during both approach to flare-out and departure maneuvers. For altitudes above flare-out, the system sums the instantaneous coefficient of lift signals of a lift transducer with a generated signal representing ideal coefficient of lift for approach to flare-out, i.e., a value of about 30% below stall. Error signals resulting from the summation are read out by the noted tactile device. Below flare altitude, an altitude responsive variation is summed with the signal representing ideal coefficient of lift to provide error signal readout.
Semi-automatic aircraft control system
1978-06-06
Miscellaneous
No indication
English
Semi-automatic aircraft wheel testing
Tema Archive | 1981
Semi-automatic Aircraft Wheel Testing
Emerald Group Publishing | 1981
Semi-active noise control system for aircraft and aircraft
European Patent Office | 2023
|