Literature DB >> 24808521

Neural network-based optimal adaptive output feedback control of a helicopter UAV.

David Nodland, Hassan Zargarzadeh, Sarangapani Jagannathan.   

Abstract

Helicopter unmanned aerial vehicles (UAVs) are widely used for both military and civilian operations. Because the helicopter UAVs are underactuated nonlinear mechanical systems, high-performance controller design for them presents a challenge. This paper introduces an optimal controller design via an output feedback for trajectory tracking of a helicopter UAV, using a neural network (NN). The output-feedback control system utilizes the backstepping methodology, employing kinematic and dynamic controllers and an NN observer. The online approximator-based dynamic controller learns the infinite-horizon Hamilton-Jacobi-Bellman equation in continuous time and calculates the corresponding optimal control input by minimizing a cost function, forward-in-time, without using the value and policy iterations. Optimal tracking is accomplished by using a single NN utilized for the cost function approximation. The overall closed-loop system stability is demonstrated using Lyapunov analysis. Finally, simulation results are provided to demonstrate the effectiveness of the proposed control design for trajectory tracking.

Year:  2013        PMID: 24808521     DOI: 10.1109/TNNLS.2013.2251747

Source DB:  PubMed          Journal:  IEEE Trans Neural Netw Learn Syst        ISSN: 2162-237X            Impact factor:   10.451


  1 in total

1.  Single Neural Adaptive PID Control for Small UAV Micro-Turbojet Engine.

Authors:  Wei Tang; Lijian Wang; Jiawei Gu; Yunfeng Gu
Journal:  Sensors (Basel)       Date:  2020-01-08       Impact factor: 3.576

  1 in total

北京卡尤迪生物科技股份有限公司 © 2022-2023.