scholarly journals Light mirror reflection and orientational irradiation automatic tracking control model

Author(s):  
Shuying Wang ◽  
Zhanmin Yang ◽  
Yi Wang
2018 ◽  
Vol 198 ◽  
pp. 05007
Author(s):  
Xiaoyi Wang

A control model for the direct parameter approach for spacecraft attitude tracking is presented in this paper. First of all, the spacecraft attitude tracking control model is built up by the error equation of the second-order nonlinear quaternion-based attitude system. A problem of control system stabilization is raised based on the control model. Compared with other control models, the second-order can offer the advantages of noapproximation and clear control states. The basic spacecraft control model has to focus on to the two variables which are angular rate and attitude quaternion, however, the new attitude control problem is only with respect to one variable which is the spacecraft attitude quaternion. Therefore, the second-order model is simpler and clear than basic first-order model.


1990 ◽  
Author(s):  
Bobby L. Ulich ◽  
Kent P. Pflibsen ◽  
Chris Sheppard ◽  
Lonnie K. Calmes

2012 ◽  
Vol 2012 ◽  
pp. 1-11 ◽  
Author(s):  
L. Faybusovich ◽  
T. Mouktonglang

We relate a deterministic Kalman filter on semi-infinite interval to linear-quadratic tracking control model with unfixed initial condition.


2009 ◽  
Vol 2009 ◽  
pp. 1-16 ◽  
Author(s):  
Valdecir Bottega ◽  
Alexandre Molter ◽  
Jun S. O. Fonseca ◽  
Rejane Pergher

This work presents a tracking control model for a flexible nonprismatic link robotic manipulator using simultaneously motor torques and piezoelectric actuators. The dynamic model of the flexible manipulator is obtained in a closed form through the Lagrange equations. The control uses the motor torques for the joints tracking control and also to reduce the low-frequency vibration induced in the manipulator links. The stability of this control is guaranteed by the Lyapunov stability theory. Piezoelectric actuators and sensors are added for controlling vibrations with frequencies beyond the reach of motor torque control. The naturals frequencies are calculated by the finite element method, and the approximated eigenfunctions are interpolated by polynomials. Three eigenfunctions are used for the dynamics of the arm, while only two are used for the control. Numerical experiments on Matlab/Simulink are used to verify the efficiency of the control model.


2014 ◽  
Author(s):  
Melissa D. McKenzie ◽  
Sarah Ramsey ◽  
Alan Rosenbaum

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