Precise Array Response Control for Beampattern Synthesis with Minimum Pattern Distortion

2021 ◽  
pp. 108395
Author(s):  
Xiaoyu Ai ◽  
Lu Gan
2021 ◽  
pp. 103152
Author(s):  
Weilai Peng ◽  
Xuejing Zhang ◽  
Zishu He ◽  
Julan Xie ◽  
Chunlin Han

2010 ◽  
Vol 32 (2) ◽  
pp. 481-484 ◽  
Author(s):  
Liang-bing Hu ◽  
Hong-wei Liu ◽  
Xiao-chao Yang ◽  
Shun-jun Wu

Impact ◽  
2019 ◽  
Vol 2019 (10) ◽  
pp. 73-75
Author(s):  
Susumu Hara

Professor Susumu Hara is based at the Department of Aerospace Engineering, Nagoya University in Japan explains that when the Mars rover Opportunity was set to land on that planet in the first weeks of 2004, onlookers held their breath as it dropped from orbit and hurtled toward the red surface. 'Any failure in the calculations or landing systems would mean a harder than expected impact,' he highlights. 'The impacts sustained by a rover such as Opportunity can derail a mission before it even starts, damaging cargo or vital systems required to complete the mission.' Impacts occur during landing but also as the craft enters the atmosphere, when it makes sudden moves, while it is on surface or when debris strikes it. 'Therefore, a system and materials to protect a craft are vital,' outlines Hara. 'Surprisingly, the solutions to this problem are not sophisticated. In fact, most craft still employ devices resembling automobile bumpers, which absorb the energy from an impact by crumpling under the force of said impact.' Unfortunately, these cannot be reused, even during testing phases a new prototype is required after every single test run. Recent missions also employed techniques like airbags or sky cranes. While successful they too have drawbacks. 'Airbags create huge rebounds which can jostle the craft and the contents inside while sky cranes are extremely costly to develop,' Hara says. For this reason, he is dedicated to designing a new highly reliable and cost-effective shock control mechanism.


2017 ◽  
Vol 17 (03) ◽  
pp. 1750039 ◽  
Author(s):  
Kenan Yildirim ◽  
Seda G. Korpeoglu ◽  
Ismail Kucuk

Optimal boundary control for damping the vibrations in a Mindlin-type beam is considered. Wellposedness and controllability of the system are investigated. A maximum principle is introduced and optimal control function is obtained by means of maximum principle. Also, by using maximum principle, control problem is reduced to solving a system of partial differential equations including state, adjoint variables, which are subject to initial, boundary and terminal conditions. The solution of the system is obtained by using MATLAB. Numerical results are presented in table and graphical forms.


2020 ◽  
pp. 102901
Author(s):  
Huake Wang ◽  
Guisheng Liao ◽  
Yuhong Zhang ◽  
Jingwei Xu ◽  
Shengqi Zhu ◽  
...  

2021 ◽  
Vol 69 (1) ◽  
pp. 182-194
Author(s):  
Lifang Feng ◽  
Guolong Cui ◽  
Xianxiang Yu ◽  
Lingjiang Kong

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