Title :
Research on starting clutch control strategy of unmanned helicopter
Author :
Zhou Yaoming ; Zhang Lei ; Xu Hongzhe ; Wu Zhe
Author_Institution :
Sch. of Aeronaut. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Abstract :
A method is explored to realize automatic control of starting clutch. The clutch control requirements are determined based on the dynamics characteristics research of an unmanned helicopter clutch, and the analysis of clutch engagement process effect on transmission impact and belts life. The rotating speed of clutch driving pulley and driven pulley are selected as basic input parameters. The starting clutch engagement control is divided into three stages. The three stages are fast engagement before rotor rotates, slow engagement and fast engagement after synchronization in turn. Subsection algorithm is adopted in fast engagement before rotor rotates. PID algorithm is adopted in slow engagement. The automatic control of starting clutch engagement at various operating conditions is realized in this way. The experimental results indicate that this control strategy can fit the changes of clutch parameters. It is proved that this clutch control strategy has met the autonomous control requirements of unmanned helicopter.
Keywords :
aircraft control; autonomous aerial vehicles; clutches; helicopters; synchronisation; three-term control; PID algorithm; belt life; clutch control requirement; clutch parameter; dynamics characteristics; rotating speed; rotor; starting clutch control strategy; starting clutch engagement control; subsection algorithm; synchronization; transmission impact; unmanned helicopter; unmanned helicopter clutch; Belts; Engines; Friction; Helicopters; Pulleys; Rotors; Torque; Automatic engagement; Clutch; Control strategy; Unmanned helicopter;
Conference_Titel :
Control, Automation and Systems (ICCAS), 2011 11th International Conference on
Conference_Location :
Gyeonggi-do
Print_ISBN :
978-1-4577-0835-0