Model system based on moment theory, blade element theory and FlightLab software is designed for small-size unmanned helicopter. The system includes three models of helicopter, moment theory model (MTM), blade element theory model (BETM) and FlightLab model (FLM). MTM is used mainly for performance analysis, BETM for control system design and FLM for nonlinear real-time simulation. Then a high-reliable model system is realized by analysis and compare. The model system has good effect by simulations and fly tests.
Model system design for small-size unmanned helicopter based on moment theory, blade element theory and FlightLab software
01.12.2008
581174 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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