Maneuver simulation of aircraft with thrust vector within extend flight wrap

被引：0

作者：

Su, HQ ^{[1
]}

Yu, HY ^{[1
]}

Song, SJ ^{[1
]}

Deng, JH ^{[1
]}

Ouyang, M ^{[1
]}

机构：

[1] Tsing Hua Univ, State Key Lab Safety & Energy, Beijing 100084, Peoples R China

来源：

System Simulation and Scientific Computing, Vols 1 and 2, Proceedings | 2005年

关键词：

aircraft with thrust vector; models; RHO control algorithm; simulations;

D O I：

暂无

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

Comparing with general aircraft, aircraft with thrust vector can improve its performance much more, at the other hand, it's also a challenge to search a new control algorithm to assign commands between different effectors to satisfy high flight quality within extend flight wrap. Firstly equations are showed up such as six freedom movement equations of aircraft, simplified models of thrust vector, actuator and sensor models, then Receding, Horizon Optimal( RHO) control algorithm and its solutions are deduced, at last, 3 kinds of simulations are executed to prove both thrust vector and thrust force must work together and suitably is the guarantee for aircraft flying within extend flight wrap.

引用

页码：1045 / 1050

页数：6