standoff tracking
Recently Published Documents


TOTAL DOCUMENTS

47
(FIVE YEARS 16)

H-INDEX

10
(FIVE YEARS 2)

2022 ◽  
Vol 102 ◽  
pp. 1-20
Author(s):  
Wenchuan Zang ◽  
Peng Yao ◽  
Dalei Song

2021 ◽  
pp. 905-919
Author(s):  
Yi Zhang ◽  
Guowei Fang ◽  
Xiuxia Yang ◽  
Yuanxin Wang ◽  
Xuan Yan ◽  
...  

Author(s):  
Chuanjian Lin ◽  
Jingping Shi ◽  
Yongxi Lyu ◽  
Yueping Wang

Target tracking of ground targets is a significant application of unmanned aerial vehicles (UAVs) in civil and military fields. There are two common modes for target tracking: over-flight tracking and standoff tracking. Each tracking method has a wide application prospect. However, many researchers have studied these two tracking methods separately and designed different guidance laws, which is not conducive to practical application. In this paper, a new guidance law based on sliding mode guidance (SMG) is proposed for tracking a stationary target, which is compatible with the two tracking modes. The stability and finite-time convergence of the guidance law are proved. Then, the guidance is extended to tracking a moving target. The numerical simulations are carried out for the tracking problems of ground targets, and the results verify the effectiveness of the proposed guidance law.


Author(s):  
Chuanjian Lin ◽  
Jingping Shi ◽  
Weiguo Zhang ◽  
Yongxi Lyu

2021 ◽  
pp. 1-12
Author(s):  
Yanxiang Wang ◽  
Honglun Wang ◽  
Jianfa Wu ◽  
Yiheng Liu ◽  
Yuebin Lun

2020 ◽  
Vol 14 (4) ◽  
pp. 5133-5143
Author(s):  
Xin Wei ◽  
Peng Yao ◽  
Zexiao Xie

2020 ◽  
Vol 10 (11) ◽  
pp. 3709 ◽  
Author(s):  
Fei Che ◽  
Yifeng Niu ◽  
Jie Li ◽  
Lizhen Wu

Cooperative standoff tracking of moving targets is an important application of fixed-wing unmanned aerial vehicles (UAVs). To cope with the problem of long convergence time and unstable tracking in cooperative target tracking, traditional Lyapunov vector field guidance (LVFG) is modified. The guidance parameter c is discussed, and the gradient descent method is utilized to develop the optimal guidance parameter search algorithm. As for tracking moving targets, an interacting multiple model-based unscented Kalman filter (IMM-UKF) estimator is built for predicting the target state, and the result is used for correcting the guidance law. Meanwhile, a speed-based controller is developed for faster convergence to the desired intervehicle phase, and the stability of the controller is proved using the Lyapunov stability theory. Numerical simulation results indicate the proposed guidance converges faster to the standoff circle without intersecting the orbit. The state estimator reduces the estimate error and the intervehicle phase converges faster to the desired phase than the traditional control method. Furthermore, extensive hardware-in-the-loop simulations are carried out to verify the feasibility of the algorithm.


2020 ◽  
Author(s):  
Tagir Muslimov ◽  
Rustem Munasypov

Accepted at "Nonlinearity, Information and Robotics 2020" Conference<br>


Sign in / Sign up

Export Citation Format

Share Document