Add to ORKGThe work is concerned with the optimal control and correction of a three-axis gyroscopic platform fixed on board of a flying object. The deviations from the predetermined motion are minimized by means of a method of programmed control, an algorithm of the optimal correction control, and selection of optimal parameters for the gyroscopic platform
In this paper a controller for the pitch angle of an aircraft regarding to the elevator deflection a...
The standard results of linearised optimal control theory are explored and examined to see how they ...
The work objective is the synthesis of simple analytical formula of the optimal roll angle of hypers...
The article considers the control problem of the aircraft cabin simulator with a four-axis gimbal gy...
This paper describes a Gyroscope balancing device which is gravity operated. The device is mounted a...
A control algoritm of a three-degree-of-freedom gyroscope axis motion emerging from a solution to th...
The paper presents a mathematical model of a triaxial gyroscopic platform on a moving platform base ...
The optimal control problem of the spin axis of a gyrostat is studied and solved via a direct transc...
AbstractThis paper deals with gyroscopic stabilization of platform. The platform consists of paralle...
The algorithm that calculates PID controller consists of three separate parameters, so sometimes it ...
Gyroscopic stabilization can be used to maintain an otherwise unstable body in an upright position. ...
In this paper, a 3 DOF gyrscope position control have been designed and controlled using optimal con...
[ES] Este artículo presenta una aplicación de control para la estabilización inercial de una platafo...
This work investigates the gravity compensation topic, from a control perspective. The gravity could...
This article presents the development of a mathematical model of a quadrotor platform and the design...
In this paper a controller for the pitch angle of an aircraft regarding to the elevator deflection a...
The standard results of linearised optimal control theory are explored and examined to see how they ...
The work objective is the synthesis of simple analytical formula of the optimal roll angle of hypers...
The article considers the control problem of the aircraft cabin simulator with a four-axis gimbal gy...
This paper describes a Gyroscope balancing device which is gravity operated. The device is mounted a...
A control algoritm of a three-degree-of-freedom gyroscope axis motion emerging from a solution to th...
The paper presents a mathematical model of a triaxial gyroscopic platform on a moving platform base ...
The optimal control problem of the spin axis of a gyrostat is studied and solved via a direct transc...
AbstractThis paper deals with gyroscopic stabilization of platform. The platform consists of paralle...
The algorithm that calculates PID controller consists of three separate parameters, so sometimes it ...
Gyroscopic stabilization can be used to maintain an otherwise unstable body in an upright position. ...
In this paper, a 3 DOF gyrscope position control have been designed and controlled using optimal con...
[ES] Este artículo presenta una aplicación de control para la estabilización inercial de una platafo...
This work investigates the gravity compensation topic, from a control perspective. The gravity could...
This article presents the development of a mathematical model of a quadrotor platform and the design...
In this paper a controller for the pitch angle of an aircraft regarding to the elevator deflection a...
The standard results of linearised optimal control theory are explored and examined to see how they ...
The work objective is the synthesis of simple analytical formula of the optimal roll angle of hypers...