Title :
Model system design for small-size unmanned helicopter based on moment theory, blade element theory and FlightLab software
Author :
Xiaoqing, Wang ; Yimin, Huang
Author_Institution :
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing
Abstract :
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.
Keywords :
aerospace engineering; control engineering computing; control system synthesis; helicopters; remotely operated vehicles; FlightLab software; blade element theory model; control system design; model system design; moment theory; moment theory model; nonlinear real-time simulation; small-size unmanned helicopter; Analytical models; Blades; Control system synthesis; Helicopters; Nonlinear control systems; Performance analysis; Real time systems; Software design; System analysis and design; System testing;
Conference_Titel :
Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
Conference_Location :
Shenzhen
Print_ISBN :
978-1-4244-3908-9
Electronic_ISBN :
978-1-4244-2386-6
DOI :
10.1109/ISSCAA.2008.4776285
