Autonomous Aerial Refueling Formation Flight Control Based on Finite-time Control under Wind Field Disturbance

Author(s):  
You Duan ◽  
Yaohong Qu ◽  
Wenbi Zhao
IEEE Access ◽  
2020 ◽  
Vol 8 ◽  
pp. 211401-211410
Author(s):  
Qian Zhang ◽  
Jingjuan Zhang ◽  
Xueyun Wang ◽  
Yifan Xu ◽  
Zelong Yu

2020 ◽  
Vol 25 (2) ◽  
Author(s):  
Fang Wang ◽  
Jianmei Wang ◽  
Kun Wang ◽  
Changchun Hua ◽  
Qun Zong

In this paper, the finite-time control design problem for a class of nonlinear systems with matched and mismatched uncertainty is addressed. The finite-time control scheme is designed by integrating multi power reaching (MPR) law and finite-time disturbance observer (FTDO) into integral sliding mode control, where a novel sliding surface is designed, and the FTDO is applied to estimate the uncertainty. Then the fixed-time reachability of the MPR law is analyzed, and the finite-time stability of the closed-loop system is proven in the framework of Lyapunov stability theory. Finally, numerical simulation and the application to the flight control of hypersonic vehicle (HSV) are provided to show the effectiveness of the designed controller.


Author(s):  
Kanya Rattanamongkhonkun ◽  
Radom Pongvuthithum ◽  
Chulin Likasiri

Abstract This paper addresses a finite-time regulation problem for time-varying nonlinear systems in p-normal form. This class of time-varying systems includes a well-known lower-triangular system and a chain of power integrator systems as special cases. No growth condition on time-varying uncertainties is imposed. The control law can guarantee that all closed-loop trajectories are bounded and well defined. Furthermore, all states converge to zero in finite time.


Author(s):  
Emmanuel Cruz‐Zavala ◽  
Tonametl Sanchez ◽  
Emmanuel Nuño ◽  
Jaime A. Moreno

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