DocumentCode :
3315217
Title :
Modeling and control of a novel Hybrid Ground Aerial Robot
Author :
Elsamanty, Mahmoud ; Fanni, Mohamed ; Ramadan, Ahmed ; Abo-Ismail, Ahmed
Author_Institution :
Mechatron. & Robot. Eng. Dept., Egypt-Japan Univ. of Sci. & Technol., Alexandria, Egypt
fYear :
2013
fDate :
4-7 Aug. 2013
Firstpage :
1559
Lastpage :
1565
Abstract :
This paper presents the dynamic modeling and control simulation of a novel robot that combines flying motion and on ground motion into an integrated single robot. The ground motion is based on four wheels configuration that provides more stability. The flying motion is depending on the flying mechanism of quadrotor system. Smart transformation mechanism is developed to switch the robot from the ground motion configuration to the flying motion configuration and vice versa without adding any additional actuators. A manipulator with 3 DOF is added to handle an object during the ground motion and it is useful to hold this object during the flying motion. A CAD model is developed using SOLIDWORKS. The dynamic model of this robot is derived to achieve the eccentricity of the payload, the weight of the eccentric manipulator and managing the variation of the payload in the dynamic model. The derived robot dynamics are highly nonlinear. A controller is designed based on feedback linearization technique to stabilize the robot attitude and altitude. Controlling the horizontal movements´ nonholonomic constraints is used to generate the desired trajectories of robot attitudes. Another dynamic model and controller have been established for the transformation mechanism. Finally, the simulation results using MATLAB/SIMULINK show that the controller successfully vanish the eccentric effect and stabilize the robot attitude.
Keywords :
CAD; attitude control; autonomous aerial vehicles; control engineering computing; control system synthesis; feedback; helicopters; linearisation techniques; manipulator dynamics; mechanical engineering computing; motion control; stability; wheels; CAD model; Matlab; Simulink; Solidworks software; computer aided design model; controller design; eccentric manipulator weight; feedback linearization technique; flying motion configuration; four wheels configuration; ground motion configuration; hybrid ground aerial robot; integrated single robot; manipulator; payload eccentricity; payload variation management; quadrotor system; robot altitude stabilization; robot attitude stabilization; robot control simulation; robot dynamic modeling; smart transformation mechanism; Dynamics; Force; Mathematical model; Propellers; Robots; Rotors; Solid modeling; Controller design; Dynamic Modeling of UAV; Feedback Linearization technique; Flying robot;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation (ICMA), 2013 IEEE International Conference on
Conference_Location :
Takamatsu
Print_ISBN :
978-1-4673-5557-5
Type :
conf
DOI :
10.1109/ICMA.2013.6618146
Filename :
6618146
Link To Document :
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