Abstract A possibility of evaluating dynamic response of a mechanical system to controlling actions of the automatic stabilization and control system is considered on the basis of a numerical experiment. Examples of design analysis are presented for a light-weight helicopter in which an autopilot is part of the control system. The finite element analysis is used in this paper.
Modeling of helicopter behavior dynamics under the controlling action of the stabilization and control system
Russian Aeronautics (Iz VUZ) ; 56 , 3 ; 224-228
2013-07-01
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Control System Dynamics of Helicopter
British Library Conference Proceedings | 1992
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