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
2015-10-01
7 pages
Article (Journal)
Electronic Resource
English
NTIS | 1972
Aircraft Mechanical Subsystems
NTIS | 1968
|Aircraft Mechanical Subsystems
NTIS | 1968
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