An approach to the development of a hybrid high-speed rotary-wing aircraft reconfiguration system is considered. The stages of system concept development, justification of its functionality, architecture formation and technical appearance are considered.
Concept of Hybrid Reconfiguration of High-speed Rotary-wing Aircraft Flight Control System
14.04.2022
1471722 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch