Adaptive Sliding Control of Six-DOF Flight Simulator Motion Platform

Fuzzy Sliding Mode Control of a Flight Simulator Motion Base

The purpose of this study is to apply sliding mode control integrated with fuzzy control for a six degree of freedom flight simulator motion system. Fuzzy logic control is included for reducing chattering phenomena. Forward and inverse kinematics and full dynamic model of six degrees of freedom motion base driven by electromechanical actuators are briefly presented. As a initial control design,...

Modeling, Simulation and Motion Cues Visualization of a Six-DOF Motion Platform for Micro-Manipulations

This paper examines the problem of realizing a 6-DOF motion platform by proposing a closed loop kinematic architecture that benefits from an anthropological serial manipulator design. In contrast to standard motion platforms based on linear actuators, a mechanism with actuator design inspired from anthropological kinematic structure offers a relatively larger motion envelope and higher dexterit...

Adaptive Quaternion Attitude Control of Aerodynamic Flight Control Vehicles

Conventional quaternion based methods have been extensively employed for spacecraft attitude control where the aerodynamic forces can be neglected. In the presence of aerodynamic forces, the flight attitude control is more complicated due to aerodynamic moments and inertia uncertainties. In this paper, a robust nero-adaptive quat...

Model based control of a flight simulator motion system

Application of H ∞ Theory to a 6 DOF Flight Simulator Motion Base

The purpose of this study is to apply inverse dynamics control for a six degree of freedom flight simulator motion system. Imperfect compensation of the inverse dynamic control is intentionally introduced in order to simplify the implementation of this approach. The control strategy is applied in the outer loop of the inverse dynamic control to counteract the effects of imperfect compensation. ...