A flight investigation to determine the effectiveness of an automatic aileron trim control device installed in a personal airplane to augment the apparent spiral stability has been conducted. The device utilizes a rate-gyro sensing element in order to switch an on-off type of control that operates the ailerons at a fixed rate through control centering springs. An analytical study using phase-plane and analog-computer methods has been carried out to determine a desirable method of operation for the automatic trim control.
Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device for Personal Airplanes
1957-01-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1956
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