Yiqun Zhang

Prof. Yiqun Zhang


Research Focus & Metrics

Academic Career Length

14Years (2013-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 April 2017 in Aerospace Science and Technology
Verified
Journal Article
Closed access
GYGuigeng Yang
Guigeng Yang
DYDongwu Yang
Dongwu Yang
YZYiqun Zhang
Yiqun Zhang
JDJiling Du
Jiling Du

1 January 2016 in Aerospace Science and Technology
Verified
Journal Article
Closed access
YZYiqun Zhang
Yiqun Zhang
WRWenrui Ru
Wenrui Ru
GYGuigeng Yang
Guigeng Yang
NLNa Li
Na Li

25 April 2025 in IEEE Antennas and Wireless Propagation Letters
Verified
Journal Article
Closed access
QWQUNBIAO WANG
QUNBIAO WANG
PLPeng Li
Peng Li
YZYiqun Zhang
Yiqun Zhang
GTGuodong Tan
Guodong Tan
YYYuanhang Yang
Yuanhang Yang
Paolo RoccaPaolo Rocca
Paolo Rocca
This work presents an interval analysis (IA) based method for the tolerance analysis and robust design of shaped reflector antennas generating contour beams. First, the expression of the power pattern of the contour beam is properly defined in terms of the azimuth and elevation angles and the Cartesian IA (CIA) is then used to derive the lower and upper bounds of the corresponding interval function. The reliability of the proposed CIA tolerance method is analyzed through a set of representative numerical examples including random surface deformations of the reflector surface. Finally, the Particle Swarm Optimizer (PSO) is integrated with the CIA-based interval analysis method for the robust design of shaped reflector antennas. The robustness of the obtained solutions is validated against the results from analytic Monte Carlo simulations and the commercial solver GRASP.

1 February 2015 in Aerospace Science and Technology
Verified
Journal Article
Closed access
YZYiqun Zhang
Yiqun Zhang
FGFeng Gao
Feng Gao
SZShuxin Zhang
Shuxin Zhang
JHJia Hao
Jia Hao

25 November 2016 in Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Verified
Journal Article
Closed access
PDF file
GYGuigeng Yang
Guigeng Yang
BDBaoyan Duan
Baoyan Duan
JDJingli Du
Jingli Du
YZYiqun Zhang
Yiqun Zhang
On-orbit space deployable antennas withstand periodic thermal loads, which will degrade the antenna surface accuracy. Thus, it is necessary to preliminarily adjust the antenna before launch to make it adapt to the space temperature environment as much as possible. Aiming at this problem, a pre-adjustment method based on min-max concept is presented in this study. First, according to the force equilibrium equation of the cable element, the incremental equilibrium equation of the cable mesh antenna is derived, and the incremental expressions of the reflector's surface displacement and cable tension with respect to cable length variation and element temperature variation are also developed. Then, the optimization model for shape pre-adjustment is established using min-max method, and the pre-adjustment process is implemented by sequence planning strategy. Finally, an AstroMesh antenna is employed to demonstrate the validity of the method.

1 May 2016 in Mechatronics
Verified
Journal Article
Closed access
YZYiqun Zhang
Yiqun Zhang
DYDongwu Yang
Dongwu Yang
SLSunlan Li
Sunlan Li