Intelligent Auto pilot Design for a Nonlinear Model of an Autonomous Helicopter by Adaptive Emotional Approach

Authors

Abstract:

There is a growing interest in the modeling and control of model helicopters using nonlinear dynamic models and nonlinear control. Application of a new intelligent control approach called Brain Emotional Learning Based Intelligent Controller (BELBIC) to design autopilot for an autonomous helicopter is addressed in this paper. This controller is applied to a nonlinear model of a helicopter. This methodology has been previously proved to present robust characteristics against disturbances and uncertainties existing in the system. The simulation results of this controller has compared with a PID controller. The policies for PID and BELBIC controller are the same. The controller design goal is that the helicopter tracks a special maneuver to reach the commanded height and heading. The performance of the controllers is also evaluated for robustness against perturbations with inserting a high frequency disturbance. Simulation results show a desirable performance in both tracking and improved control signal by using BELBIC controller.

Upgrade to premium to download articles

Sign up to access the full text

Already have an account?login

similar resources

investigating the feasibility of a proposed model for geometric design of deployable arch structures

deployable scissor type structures are composed of the so-called scissor-like elements (sles), which are connected to each other at an intermediate point through a pivotal connection and allow them to be folded into a compact bundle for storage or transport. several sles are connected to each other in order to form units with regular polygonal plan views. the sides and radii of the polygons are...

Auto - Pilot : Autonomous Control of a remote controlled helicopter

An auto-pilot system was created which could track and control a Syma S107 RC mini infrared helicopter in real-time. The helicopter was tracked using two LEDs attached to it, one situated on the front of the helicopter and one situated on the tail. Image processing and object tracking algorithms were used to track the position of the helicopter. In order to perform real-time tracking, the metho...

full text

Electronics Design for an Autonomous Helicopter by Christian A . Trott

Over a two year period, two generations of electronics hardware for a fully functional autonomous aerial vehicle have been developed. Both custom-designed and off-the-shelf components have been integrated on a small radio controlled helicopter. This vehicle, the Draper Small Autonomous Aerial Vehicle (DSAAV), is now capable of fully autonomous take-off, way-point guidance, vision processing and...

full text

A Simulation Model of An Autonomous Helicopter

This paper describes a simulation model that has been used for controller design and stability and performance analysis of a micro X-CELL helicopter as central element of the Autonomous Scout Rotorcraft Testbed (ASRT) developed at Georgia Institute of Technology, Atlanta, USA. The general model, simple, yet comprehensive and efficient for the task at hand, consists of the following elements: he...

full text

A comparative design of a MIMO neural adaptive rate damping for a nonlinear helicopter model

Using a nonlinear 15-state helicopter model in 6 DOF, two di erent neural control systems, both acting as rate damping, have been designed and compared. They are both based on the reference model direct inverse scheme, but they di er each from the other for the identi cation of the inverse model: the rst one is a MIMO feedforward two-layered neural network, while the second one is a combination...

full text

A Comprehensive Study of Control Design for an Autonomous Helicopter

In this paper, we compare three different control methodologies for helicopter autopilot design: linear robust multi-variable control, fuzzy logic control with evolutionary tuning, and nonlinear tracking control. The control design is based on nonlinear dynamic equations with a simplified thrust-torque generation model valid for hovering and low velocity flight. We verify the controller perform...

full text

My Resources

Save resource for easier access later

Save to my library Already added to my library

{@ msg_add @}


Journal title

volume 9  issue 2

pages  -

publication date 2633-07-23

By following a journal you will be notified via email when a new issue of this journal is published.

Hosted on Doprax cloud platform doprax.com

copyright © 2015-2023