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. The control strategy is designed using H-infinity theory. Forward and inverse kinematics and full dynamic model of a six degrees of freedom motion base driven by electromechanical actuators are briefly presented. Describing function, acceleration step response and some maneuvers computed from the washout filter were used to evaluate the performance of...
This paper describes the use of inverse simulation to develop feedforward controllers for model-bas...
AbstractThere is proposed an adaptive sliding controller in task space on the base of the linear New...
There is a significant interest in developing flight control laws which need minimum gain scheduling...
The purpose of this study is to apply inverse dynamics control for a six degree of freedom flight si...
The purpose of this study is to apply inverse dynamics control for a six degree of freedom flight si...
The purpose of this study is to apply robust inverse dynamics control for a six-degree-of-freedom fl...
The modern trend of developing highly automated aircraft is characterized by a transition from tradi...
The inertial response characteristics of a synergistic, six-degree-of-freedom motion base are presen...
The inertial response characteristics of a synergistic, six-degree-of-freedom motion base are presen...
Abstract: This paper focuses on a detailed description and application of inverse simulation, which ...
Good motion cueing in a flight simulator serves to enhance the overall simulation environment. Howev...
Typically, the spacecraft model has high uncertainties and the dynamic inverse inner loop controller...
Aircraft control normally relies on gain-scheduling of linear control laws, an approach that has bee...
Following extensive development over the past two decades, techniques of inverse simulation have led...
Inverse simulation is becoming more and more popular and widely used technique in flight mechanics s...
This paper describes the use of inverse simulation to develop feedforward controllers for model-bas...
AbstractThere is proposed an adaptive sliding controller in task space on the base of the linear New...
There is a significant interest in developing flight control laws which need minimum gain scheduling...
The purpose of this study is to apply inverse dynamics control for a six degree of freedom flight si...
The purpose of this study is to apply inverse dynamics control for a six degree of freedom flight si...
The purpose of this study is to apply robust inverse dynamics control for a six-degree-of-freedom fl...
The modern trend of developing highly automated aircraft is characterized by a transition from tradi...
The inertial response characteristics of a synergistic, six-degree-of-freedom motion base are presen...
The inertial response characteristics of a synergistic, six-degree-of-freedom motion base are presen...
Abstract: This paper focuses on a detailed description and application of inverse simulation, which ...
Good motion cueing in a flight simulator serves to enhance the overall simulation environment. Howev...
Typically, the spacecraft model has high uncertainties and the dynamic inverse inner loop controller...
Aircraft control normally relies on gain-scheduling of linear control laws, an approach that has bee...
Following extensive development over the past two decades, techniques of inverse simulation have led...
Inverse simulation is becoming more and more popular and widely used technique in flight mechanics s...
This paper describes the use of inverse simulation to develop feedforward controllers for model-bas...
AbstractThere is proposed an adaptive sliding controller in task space on the base of the linear New...
There is a significant interest in developing flight control laws which need minimum gain scheduling...