Study of system suitable for high performance aircraft and missiles measuring vehicle response to small amplitude control surface deflections produced by sinusoidal test signal; changes in response to signal are related to environmental changes; system is continuously altered to maintain response equal to preselected value; effects on system performance of variation in flight condition, system gain level, test signal frequency, and sensor location.
Analytical investigation of adaptive flight-control system using sinusoidal test signal J
NASA -- Tech Note
1961
64 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.