Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory
Daniel J. BiezadAñadir a mi colección
Formato
Añadir a mi colección
Formato
También te puede gustar
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
Wendy B. Lessard
1996
AñadirLow-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft
Jacques C. Richard
1995
AñadirElectromagnetic on-aircraft antenna radiation in the presence of composite plates
S. H-T Kan
1994
AñadirUser's manual for interactive LINEAR, a FORTRAN program to derive linear aircraft models
Robert F. Antoniewicz
1988
Añadir