Model Derivation and Control System Simulation for Unmanned Aerial Vehicle

被引：0
|
作者：
Liu Zhiping [1 ]
Tan Fang [1 ]
机构：
[1] Xian Technol Univ, Coll Comp Sci & Engn, Xian 710032, Peoples R China
来源：
2013 25TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC) | 2013年
关键词：
Guidance and control; Simulation; UAV; Mission scenario;
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：
in this paper, a six degrees of freedom mathematical model for unmanned aerial vehicle (UAV) is proposed, in which the translational dynamics is expressed in the UAV body frame and is depicted by air velocity, angle of attack and sideslip angle. This model has the merits of explicitly formulating the dynamic states to be controlled in the system model. The simulation architecture and control system design criterion was presented. Based on the mathematical model, the mission scenario of the UAV was assigned, related uncertainties were considered, the simulation framework was constructed under the MATLAB/Simulink, the simulation results demonstrated the validity and feasibility of the proposed model and related algorithm.
引用
收藏
页码：4053 / 4057
页数：5
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