Abstract The technique for evaluating the flying qualities in the case of ground-based simulation is improved. The influence of simulator subsystem fidelity that provides the improvement of convergence between ground-based and in-flight tests, is considered.
Improvement of semi-scale simulation technique and subsystems for investigation of aircraft manual control
Russian Aeronautics (Iz VUZ) ; 58 , 4 ; 394-400
01.10.2015
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
NTIS | 1972
Aircraft Mechanical Subsystems
NTIS | 1968
|Aircraft Mechanical Subsystems
NTIS | 1968
|