Electromechanical system developed at Hamilton Standard Div of United Aircraft Corp, for Hiller L model helicopter; system is 2 axis SAS which accepts signals from pitch and roll rate gyros, modifies and amplifies signals, and drives 2 linear actuators which add to pilot' s stick input to position helicopter cyclic control surfaces.
Light helicopter stability augmentation system
Electromechanical Components Systems Design
1963
6 pages
Standard
Englisch
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