|Table of Contents|

Launching process control for propeller UAV with double booster rocket

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
2015年02期
Page:
155-160
Research Field:
Publishing date:

Info

Title:
Launching process control for propeller UAV with double booster rocket
Author(s):
Pu Huangzhong1Zhen Ziyang2Xia Man2Guo Xiaoliang1
1.Institute of UAV; 2.College of Automation Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
Keywords:
unmanned aerial vehicles flight control launching process
PACS:
V249
DOI:
-
Abstract:
The design of control system and simulation analysis of key parameters at the launching process of the propeller UAV with double booster rockets are studied.The nonlinear mathematical model of the UAV launching process is set up,and the flight attitude control system consisting of control loops of the pitch angle,the roll angle and the yaw angle is designed.Then the simulation system of the UAV launching process control system is established to verify the effectiveness of the flight control system,and the influence of construction time of the propeller engine and the construction time of maximum thrust are investigated.Simulation results show that the flight control system can guarantee the stable climbing through effective control of the UAV's attitudes,and the clutching of the propeller engine and the maximizing of the throttle opening should be realized as early as possible on the premise of safe launching.

References:

[1] 刘玉宝.无人机发射段控制律设计[D].南京:南京航空航天大学自动化学院,2009.
[2]蔡云鹏,闫建国,王亮.无人机发射过程建模与控制方法研究[J].飞行力学,2010,28(1):80-83.
Cai Yunpeng,Yan Jianguo,Wang Liang.Study of control law and modeling on unmanned air vehicle launching process[J].Flight Mechanics,2010,28(1):80-83.
[3]陈怦,赵涛,王建培.无人机发射过程仿真与参数敏感性分析[J].飞行力学,2002,20(1):21-24.
Chen Peng,Zhao Tao,Wang Jianpei.Simulation of unmanned air vehicle launching process and its sensitivity analysis[J].Flight Mechanics,2002,20(1):21-24.
[4]裴锦华,吴泊宁.大型无人机双发火箭助推发射技术的研究[J].南京航空航天大学学报,1999,31(3):342-345.
Pei Jinhua,Wu Poning.Research on launching technology for heavy pilotless aircraft with double booster rockets[J].Journal of Nanjing University of Aeronautics and Astronautics,1991,31(3):342-345.
[5]Ni Shaobo,Shan Jiayuan.Smooth second-order nonsingular terminal sliding mode control for reusable launch vehicles[J].International Journal of Intelligent Computing and Cybernetics,2014,7(1):95-110.
[6]赵志鸿.某型无人机双发火箭助推发射动力学建模与仿真研究[D].南京:南京理工大学机械工程学院,2009.
[7]杨斐.无人机实时飞行仿真系统的设计与实现[D].南京:南京航空航天大学航空宇航学院,2009.
[8]吴森堂,费玉华.飞行控制系统[M].北京:北京航空航天大学出版社,2005.
[9]浦黄忠,甄子洋,黄国勇,等.变推力轴线无人机的混合姿态控制[J].南京理工大学学报,2010,34(5):596-601.
Pu Huangzhong,Zhen Ziyang,Huang Guoyong,et al.Hybrid attitude control for variable thrust axis based UAV[J].Journal of Nanjing University of Science and Technology,2010,34(5):596-601.

Memo

Memo:
-
Last Update: 2015-04-30