Abstract This work proposes a technique for simulation of integral loads created by a hingeless helicopter rotor, which is based on implementing neural network algorithms. A method, which accounts for variation of angular speeds of the main rotor in the simulation model is proposed. Feasibility of the proposed model is justified on an example of computation and simulation of a helicopter operating in steady flight conditions.
Simulation model of loads created by a hingeless helicopter rotor
Russian Aeronautics (Iz VUZ) ; 58 , 2 ; 167-172
2015-04-01
6 pages
Article (Journal)
Electronic Resource
English
Simulation model of loads created by a hingeless helicopter rotor
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