scholarly journals Performance Evaluation of Target Detection with a Near-Space Vehicle-Borne Radar in Blackout Condition

Sensors ◽  
2016 ◽  
Vol 16 (1) ◽  
pp. 64 ◽  
Author(s):  
Yanpeng Li ◽  
Xiang Li ◽  
Hongqiang Wang ◽  
Bin Deng ◽  
Yuliang Qin
2015 ◽  
Vol 8 (8) ◽  
pp. 409-424 ◽  
Author(s):  
Zhenyu Lu ◽  
Kai Li ◽  
Tingya Yang ◽  
Wei Guo ◽  
Jin Wang

2011 ◽  
Vol 128-129 ◽  
pp. 979-984
Author(s):  
Shao Bo Ni ◽  
Wei Jun Hu ◽  
Song Xiong

A de-couple control method with information feedback from other control channel and a method with double control loops were present for the hypersonic vehicle with non-linear, couple and lateral maneuver. The whole controller was divided into two parts: the computation of actuator which deal with control couple and design of control law which solve the problem of movement and aerodynamic couple. The time-varying controller parameter method and robust control law were present to solve the problem of quick time-varying model parameter and non-linear. Finally these two methods were analyzed contrastively; the simulation result show that these two methods present above can achieve the quick dynamic and high precise track of command. But the latter was better.


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