TY - GEN
T1 - Pointing behavior of perimeter truss deployable antenna with a laminated reflector
AU - Yiming, Sun
AU - Bindi, You
AU - Peibo, Hao
AU - Dong, Liang
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/7/2
Y1 - 2017/7/2
N2 - Perimeter Truss Deployable Antenna reflector is made of laminated circular plates. The laminated plate would be deformed when it undergoes a large angle rotational motion, and a complex geometric nonlinearity problem would be caused by the coupling effect between the elastic deformation and a large angle rotational motion. According to such reasons, a model of laminated plate which is undergoing a large angle rotational motion based on the high-order shear deformation theory was built. At the same time, we also consider laminated structural parameters and constitutive relations of the plate. And the coupling relation between elastic deformation was analyzed and a large angle rotational motion. Moreover, we derive the rigidflexible coupling dynamics equation using Hamilton variational principle. Furthermore, the necessity of dynamic modeling considering the laminated structure was verified by the numerical simulation.
AB - Perimeter Truss Deployable Antenna reflector is made of laminated circular plates. The laminated plate would be deformed when it undergoes a large angle rotational motion, and a complex geometric nonlinearity problem would be caused by the coupling effect between the elastic deformation and a large angle rotational motion. According to such reasons, a model of laminated plate which is undergoing a large angle rotational motion based on the high-order shear deformation theory was built. At the same time, we also consider laminated structural parameters and constitutive relations of the plate. And the coupling relation between elastic deformation was analyzed and a large angle rotational motion. Moreover, we derive the rigidflexible coupling dynamics equation using Hamilton variational principle. Furthermore, the necessity of dynamic modeling considering the laminated structure was verified by the numerical simulation.
KW - dynamic modeling
KW - flexible reflector
KW - laminated plate
KW - large angle rotation
KW - non-liner deformation
UR - https://www.scopus.com/pages/publications/85049118071
U2 - 10.1109/ICCIS.2017.8274798
DO - 10.1109/ICCIS.2017.8274798
M3 - 会议稿件
AN - SCOPUS:85049118071
T3 - 2017 IEEE International Conference on Cybernetics and Intelligent Systems, CIS 2017 and IEEE Conference on Robotics, Automation and Mechatronics, RAM 2017 - Proceedings
SP - 339
EP - 344
BT - 2017 IEEE International Conference on Cybernetics and Intelligent Systems, CIS 2017 and IEEE Conference on Robotics, Automation and Mechatronics, RAM 2017 - Proceedings
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 8th IEEE International Conference on Cybernetics and Intelligent Systems, CIS 2017 and IEEE Conference on Robotics, Automation and Mechatronics, RAM 2017
Y2 - 19 November 2017 through 21 November 2017
ER -