Robust terminal angle constraint guidance law with autopilot lag for intercepting maneuvering targets

2015 ◽  
Vol 81 (1-2) ◽  
pp. 881-892 ◽  
Author(s):  
Shaoming He ◽  
Defu Lin ◽  
Jiang Wang
Author(s):  
Peng Zhang ◽  
Xiaoyu Zhang

This paper introduces a fast fixed-time guidance law with terminal angle constraint for interception of maneuvering targets, which is based on the structure of singularity-free fast terminal sliding mode and the fixed-time stability theory. Different from the finite-time stability, the fixed-time stability can predefine the maximum stabilization time of system states which is independent on the initial value of system states. Under the proposed guidance law, the guidance system can achieve stabilization within settling time which decides by the parameters of controller. In addition, an adaptive law is proposed which alleviate the chattering of sliding mode and smooths the guidance law. Meanwhile, the proof of the sliding mode manifold and system states fixed-time convergence is given by Lyapunov stability theory. Finally, numerical simulations demonstrate the performance of the proposed guidance law is satisfying.


2022 ◽  
Author(s):  
Prajapati D. Dharmendrabhai ◽  
Akash Gholap ◽  
Nikhil K. Singh ◽  
Sikha Hota

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