This paper presents a new concept and technique for solving the problems associated with the prediction and control of flight component failures which are attributed to contamination of the power transmission fluid in the servo actuating subsystem. Basically this technique assumes that these failures are probabilistic. Mathematical models are then established and comparisons made between calculated and measured values of contamination in a system to determine the degree of acceptability of the fluid.
Criteria for Contamination Level in Flight Control Systems
Sae Technical Papers
National Air Transportation Meeting ; 1968
1968-02-01
Aufsatz (Konferenz)
Englisch
Design criteria for optimal flight control systems
AIAA | 1979
|Design Criteria Multi-Loop Flight Control Systems
NTIS | 1986
|Design Criteria for Optimal Flight Control Systems
AIAA | 1980
|Design Criteria for Multi-Loop Flight Control Systems
NTIS | 1986
|British Library Conference Proceedings | 2013
|