Publication Date:
2019-06-27
Description:
A method is suggested for predicting the stability of automatically controlled aircraft by a comparison of calculated frequency-response curves for the aircraft and experimentally determined frequency-response curves for the automatic pilot. The method is applied only to stabilization in roll. The method is expected to be useful as a means of establishing the specifications of the performance required of the automatic control device for pilotless aircraft designed as missiles.
Keywords:
AERODYNAMICS
Type:
TN-1901
,
Collected Works of Robert T. Jones; p 515-532
Format:
text
Permalink