Dynamics Modeling and Analysis of Thrust-Vectored V/STOL Aircraft

被引：0

作者：

Wang Xiangyang ^{[1
]}

Zhu Jihong ^{[2
]}

Zhang Yijun ^{[3
]}

机构：

[1] Tsinghua Univ, Sch Aerosp & Aeronaut, Beijing 100084, Peoples R China

[2] Tsinghua Univ, Dept Comp Sci & Technol, Beijing 100084, Peoples R China

[3] Lanzhou Jiaotong Univ, Sch Mechatron Engn, Lanzhou 730070, Peoples R China

来源：

2013 32ND CHINESE CONTROL CONFERENCE (CCC) | 2013年

关键词：

V/STOL aircraft; vectored thrust; jet-induced effect; dynamic modeling;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

V/STOL aircrafts have different flight modes, including conventional mode, hover and transition flight. And the control effectors include thrust engines, thrust vectors and aerodynamic actuators. The dynamic model of V/STOL aircrafts varies significantly due to jet-induced effect during hover and transition flight. In this paper, dynamic model of V/STOL aircraft propulsion system and jet-induced forces are built. The 6-DOF nonlinear equations of motion, for a V/STOL UAV are formulated and simulated. Simulations results validate the dynamic model built in this paper. And the dynamic model could be used for propulsion system and control system design.

引用

页码：1825 / 1830

页数：6

共 8 条

[1] [Anonymous], 2010, P 8 WORLD C INT CONT, P85
[2] Bordignon K, 2002, BIENN INT POW LIFT C
[3] Buchholz Mark D., 2002, BIENN INT POW LIFT C
[4] Franklin J.A., 1997, NASATM112208, P1
[5] Kuhn R.E., 2006, Jet-Induced Effects: The Aerodynamics of Jet and Fan-Powered V/STOL Aircraft in Hover and Transition
[6] Price H, 1995, NASA TECHNICAL REPOR, V124, P109
[7] Walker Gregory P., 2002, BIENN INT POW LIFT C
[8] Transition flight control of two vertical/short takeoff and landing aircraft
Yang Xili
Fan Yong
Zhu Jihong
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (02) : 371 - 385

← 1 →