z-logo
open-access-imgOpen Access
Stability Control Structure of Hovercraft Prototype Utilising PID Controller
Author(s) -
Bhaskara Rao. Yenugula,
Md. Zia-ur-Rahman
Publication year - 2017
Publication title -
bulletin of electrical engineering and informatics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.251
H-Index - 12
ISSN - 2302-9285
DOI - 10.11591/eei.v6i4.864
Subject(s) - setpoint , pid controller , engineering , controller (irrigation) , inertial measurement unit , position (finance) , control theory (sociology) , automotive engineering , marine engineering , control (management) , simulation , control engineering , computer science , aerospace engineering , temperature control , artificial intelligence , agronomy , finance , economics , biology
Hovercraft is a method of transportation as an option for clients who remain on the waterway and swamp surface. The issue with hovercraft is when dubious climate and natural condition, e.g. wind speed and wave tallness exasperate solidness of hovercraft to jeopardise the driver. We propose an approach to keep up adjust of the hovercraft by controlling the focal point of gravity (PG) to be determined position. The controller monitors the position of load to change the position. A 6-DOF IMU Sensor MPU 6050 was utilised to create information as an examination with setpoint. PID control strategy was employed. The test outcome demonstrates that the model of air cushion vehicle could keep its adjust the axis orientation of the roll in spite of the fact that it was less compelling in the pitch pivot direction.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom