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

fYear

2008

fDate

10-12 Dec. 2008

Firstpage

1

Lastpage

4

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;

fLanguage

English

Publisher

ieee

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

Type

conf

DOI

10.1109/ISSCAA.2008.4776285

Filename

4776285