The Community for Technology Leaders
RSS Icon
Subscribe
Los Angeles, California USA
Mar. 31, 2009 to Apr. 2, 2009
ISBN: 978-0-7695-3507-4
pp: 187-191
ABSTRACT
Modeling of power system plays an important part in modeling of helicopter dynamics system. The precision of turbo-shaft engine model affects directly the fidelity of power system model in process of modeling and simulation on helicopter. Modeling techniques of turbo-shaft engine are studied first, secondly, engine control system model based on main rotor load feedback is proposed and an inner-outer series-wound control loop to adjust engine output power based on feedback control is developed. The control law of turbo-shaft engine power adjustment is designed. Consequently, integrative model of turbo-shaft engine and main rotor on helicopter power system is realized. A simulation example for helicopter power system is given in this paper to validate the integrative model.
INDEX TERMS
helicopter, rotor, turbo-shaft engine, simulation model
CITATION
Ma Shi-dong, Han Liang, Gong Guang-hong, Song Xiao, "Researches on Modeling and Simulation of Turbo-Shaft Engine and Main Rotor System", CSIE, 2009, Computer Science and Information Engineering, World Congress on, Computer Science and Information Engineering, World Congress on 2009, pp. 187-191, doi:10.1109/CSIE.2009.387
20 ms
(Ver 2.0)

Marketing Automation Platform Marketing Automation Tool