Modification of a helicopter inverse simulation to include an enhanced rotor model

被引：13

作者：

Doyle, SA ^{[1
]}

Thomson, DG ^{[1
]}

机构：

[1] Univ Glasgow, Dept Aerosp Engn, Glasgow G12 8QQ, Lanark, Scotland

来源：

JOURNAL OF AIRCRAFT | 2000年 / 37卷 / 03期

关键词：

Helicopter rotor blades;

D O I：

10.2514/2.2633

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

An engine governor model has been incorporated into the individual blade rotor model Hibrom for helicopter inverse simulation. The rotorspeed is now a degree of freedom within the modeled system. A series of modification has been made to the solution algorithm Genisa to accommodate the variation of rotorspeed. In particular, the control application interval is recalculated iteratively at each time step.

引用

页码：536 / 538

页数：3