TY - JOUR
T1 - Design, control, and dynamic simulation of securing and transformation mechanisms for a hybrid ground aerial robot
AU - Salman, Maha
AU - Sameh, Ahmed
AU - Fanni, Mohamed
AU - Sugano, Shigeki
AU - Mohamed, Abdelfatah M.
N1 - Funding Information:
The first author is supported by a scholarship from the Ministry of Higher Education of the Government of Egypt which is gratefully acknowledged. Also, the first author takes the permission from Electronic Research Institute to study in E-JUST.
Publisher Copyright:
© April 2020 IJENS.
PY - 2020
Y1 - 2020
N2 - A hybrid ground aerial robot (HGAR) has been developed to combine both capabilities of aerial robots and ground mobile robots to overcome the limitations of each single type. This research introduces a new securing mechanism and improves also the propeller-thruster transformation mechanism for the HGAR. The securing mechanism is designed to be light and to give high stability, and low power consumption for both flying and ground motion modes. In the developed transformation mechanism, the robot uses the propellers which are already installed for the aerial mission as actuators to transform between the flight and ground-motion configurations. In contrast to the previous design, no need here to additional position controller to avoid propellers' collision or springs to start the switch to the ground configuration. The propellers are controlled by the Feedback-Linearization which is combined with Robust-Internal Compensator to achieve the controller robustness. The HGAR is virtually built and dynamically modeled using ADAMS® software then connected with MATLAB/Simulink® to test the proposed mechanisms and the proposed controller. The results indicate a satisfactory performance of the proposed mechanisms and controller.
AB - A hybrid ground aerial robot (HGAR) has been developed to combine both capabilities of aerial robots and ground mobile robots to overcome the limitations of each single type. This research introduces a new securing mechanism and improves also the propeller-thruster transformation mechanism for the HGAR. The securing mechanism is designed to be light and to give high stability, and low power consumption for both flying and ground motion modes. In the developed transformation mechanism, the robot uses the propellers which are already installed for the aerial mission as actuators to transform between the flight and ground-motion configurations. In contrast to the previous design, no need here to additional position controller to avoid propellers' collision or springs to start the switch to the ground configuration. The propellers are controlled by the Feedback-Linearization which is combined with Robust-Internal Compensator to achieve the controller robustness. The HGAR is virtually built and dynamically modeled using ADAMS® software then connected with MATLAB/Simulink® to test the proposed mechanisms and the proposed controller. The results indicate a satisfactory performance of the proposed mechanisms and controller.
KW - Feedback linearization
KW - Hybrid ground aerial robot
KW - Internal compensator
KW - Securing mechanism
KW - Transformation mechanism
UR - http://www.scopus.com/inward/record.url?scp=85088267499&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85088267499&partnerID=8YFLogxK
M3 - Article
AN - SCOPUS:85088267499
SN - 2227-2771
VL - 20
SP - 100
EP - 107
JO - International Journal of Mechanical and Mechatronics Engineering
JF - International Journal of Mechanical and Mechatronics Engineering
IS - 2
ER -