Vargas Alvarado 2020a - Revision history

Fjvargas at 11:01, 22 June 2020

2020-06-22T11:01:10Z

Fjvargas at 14:05, 19 June 2020

2020-06-19T14:05:28Z

Fjvargas at 16:08, 11 June 2020

2020-06-11T16:08:45Z

Fjvargas at 16:06, 11 June 2020

2020-06-11T16:06:31Z

Fjvargas at 16:05, 11 June 2020

2020-06-11T16:05:47Z

Fjvargas at 16:04, 11 June 2020

2020-06-11T16:04:35Z

Fjvargas at 16:02, 11 June 2020

2020-06-11T16:02:47Z

Fjvargas at 16:00, 11 June 2020

2020-06-11T16:00:08Z

Fjvargas at 15:59, 11 June 2020

2020-06-11T15:59:14Z

Fjvargas at 15:58, 11 June 2020

2020-06-11T15:58:26Z

@@ Line 549: / Line 549: @@
 [19] D. Siqueira, F. J. Oliveira Moreira and Pedro Paglione, “Robust Flight Control Design Supported by Flying Qualities Analysis”, AIAA Guidance, Navigation and Control Conference, South Carolina, pp. 415-428, 2007. <div id="cite-19"></div>
-[20] F. J. Triveño Vargas and E. O. Pozo Irusta, “ Modelado, Simulación y Control de Sistemas Mecatronicos y Aeroespacialescon Matlab-Simulink® y Mathematica<math display="inline">^{TM}</math> ”, Editorial Serrano, 2014.
+[20] F. J. Triveño Vargas and E. O. Pozo Irusta, “ Modelado, Simulación y Control de Sistemas Mecatronicos y Aeroespaciales con Matlab-Simulink® y Mathematica<math display="inline">^{TM}</math> ”, Editorial Serrano, 2014.
 [21] W. A. Wolovich,“Automatic Control Systems: Basic Analysis and Design”, Oxford University Press, 1994.
 [22] H. Siles Alvarado, “Simulaciones en Ciencias y Tecnologia”, http://www.simcyt.org, Accessed: 2019-09-14, 2019.

@@ Line 310: / Line 310: @@
 ==5 AUTOMATIC CONTROL PROBLEM==
-The analysis and synthesis are performed by applying theory of optimal control and the technique of Linear Quadratic Regulator (LQR), method based on the linearization of dynamic systems, represented in the time domain [10, 12]. The control structure is presented in Figure [[#img-8|8]] . <div id='img-8'></div>
+The analysis and synthesis are performed by applying theory of optimal control and the technique of Linear Quadratic Regulator (LQR), method based on the linearization of dynamic systems, represented in the time domain [10, 12]. The control structure is presented in Figure [[#img-8|8]]. <div id='img-8'></div>
 {| class="floating_imageSCP" style="text-align: center; margin: 1em auto; width: 100%;max-width: 100%;"
 |-
@@ Line 507: / Line 507: @@
 ==ACKNOWLEDGMENT==
-Thanks you to the participating universities, teachers and students who made possible this publication. Also, thank you to Juan Poma Rosas for English corrections and to SIB and CIEE of Cochabamba Bolivia for the financial support
+Thanks you to the participating universities, teachers and students who made possible this publication. Also, thank you to Juan Poma Rosas for English corrections and to SIB and CIEE of Cochabamba Bolivia for the financial support.
 ==REFERENCES==
-[1] D. Deming and K. Noray, “ STEM Careers and Technological Change”, Harvard University, 2018.
+[1] D. Deming and K. Noray, “STEM Careers and Technological Change”, Harvard University, 2018.
 [2] J. Cortes Lopez and L. Jordar Sanches, “Introducción al Mathematica 7”, Universidad Politecnica de Valencia, 2011.
@@ Line 535: / Line 535: @@
 [12] K. Ogata, “Engenharia de Controle Moderno”, Pearson Educaton, 5th Edition, 2011.
-[13]  E. L. Duke and R. F. Antoniewicz and Keith D. Krambeer,  “Derivation and Definition of a Linear Aircraft Model ”,  NASA Reference Publication 1207, 1988.
+[13]  E. L. Duke and R. F. Antoniewicz and Keith D. Krambeer,  “ Derivation and Definition of a Linear Aircraft Model ”,  NASA Reference Publication 1207, 1988.
-[14] D. Gangsaas, J. Hodgkinson and C. Harden, “ Multidisciplinary Control Law Design and Flight Test Demonstration on a  Business Jet”, AIAA Guidance, Navigation and Control Conference and Exhibit pp. 1-25, 2008.
+[14] D. Gangsaas, J. Hodgkinson and C. Harden, “ Multidisciplinary Control Law Design and Flight Test Demonstration on a  Business Jet ”, AIAA Guidance, Navigation and Control Conference and Exhibit pp. 1-25, 2008.
 [15] J. Kusalaas ,“ Numerical Methods in Engineering with Python 3”, Cambridge University Press, 2013.
@@ Line 549: / Line 549: @@
 [19] D. Siqueira, F. J. Oliveira Moreira and Pedro Paglione, “Robust Flight Control Design Supported by Flying Qualities Analysis”, AIAA Guidance, Navigation and Control Conference, South Carolina, pp. 415-428, 2007. <div id="cite-19"></div>
-[20] F. J. Triveño Vargas and E. O. Pozo Irusta, `` Modelado, Simulación y Control de Sistemas Mecatronicos y Aeroespacialescon Matlab®y Mathematica<math display="inline">^{TM}</math> '', Editorial Serrano, 2014.
+[20] F. J. Triveño Vargas and E. O. Pozo Irusta, “ Modelado, Simulación y Control de Sistemas Mecatronicos y Aeroespacialescon Matlab-Simulink® y Mathematica<math display="inline">^{TM}</math> ”, Editorial Serrano, 2014.
-[21] W. A. Wolovich,“Automatic Control Systems: Basic Analysis and Design ”, Oxford University Press, 1994.
+[21] W. A. Wolovich,“Automatic Control Systems: Basic Analysis and Design”, Oxford University Press, 1994.
-[22] H. Siles Alvarado, “ Simulaciones en Ciencias y Tecnologia ”, http://www.simcyt.org, Accessed: 2019-09-14, 2019.
+[22] H. Siles Alvarado, “Simulaciones en Ciencias y Tecnologia”, http://www.simcyt.org, Accessed: 2019-09-14, 2019.

@@ Line 545: / Line 545: @@
 [17] F. J. Triveño Vargas and Pedro Paglione, “ Aplicações de Modelagem, Simulação e Controle Com Ferramentas de Algebra Computacional ”, Editorial LTC, 2015.
-[18] J. E. Villate, “Simulações com VPython”, https://def.fe.up.pt/python/vpython.html,Accessed: 2018-15-11, 2018.
+[18] J. E. Villate, “Simulações com VPython”, https://def.fe.up.pt/python/vpython.html, Accessed: 2018-15-11, 2018.
 [19] D. Siqueira, F. J. Oliveira Moreira and Pedro Paglione, “Robust Flight Control Design Supported by Flying Qualities Analysis”, AIAA Guidance, Navigation and Control Conference, South Carolina, pp. 415-428, 2007. <div id="cite-19"></div>

@@ Line 245: / Line 245: @@
 The orbit of the satellite of two degrees of freedom with mass <math display="inline">M</math> is illustrated in Figure [[#img-5|5]], can be described by two non-linear and coupled equations obtained from the sum of the kinetic energy due to the tangential component <math display="inline">v_{t} = r(t) \dot{\alpha } (t) </math> and radial component of velocity <math display="inline"> v_{r} = \dot{r}(t)</math>. It is assumed that the satellite has traction in these directions, thus the magnitude of the forces are <math display="inline">F_{t}(t)</math> and <math display="inline">F_{r}(t)</math> respectively. <div id='img-5'></div>
-{| class="floating_imageSCP" style="text-align: center; margin: 1em auto; width: 100%;max-width: 110%;"
+{| class="floating_imageSCP" style="text-align: center; margin: 1em auto; width: 110%;max-width: 110%;"
 |-
 |[[Image:Review_159642103826-labVirtSpain_20.png|150px|Two degree of freedom satellite]]

@@ Line 245: / Line 245: @@
 The orbit of the satellite of two degrees of freedom with mass <math display="inline">M</math> is illustrated in Figure [[#img-5|5]], can be described by two non-linear and coupled equations obtained from the sum of the kinetic energy due to the tangential component <math display="inline">v_{t} = r(t) \dot{\alpha } (t) </math> and radial component of velocity <math display="inline"> v_{r} = \dot{r}(t)</math>. It is assumed that the satellite has traction in these directions, thus the magnitude of the forces are <math display="inline">F_{t}(t)</math> and <math display="inline">F_{r}(t)</math> respectively. <div id='img-5'></div>
-{| class="floating_imageSCP" style="text-align: center; margin: 1em auto; width: 100%;max-width: 100%;"
+{| class="floating_imageSCP" style="text-align: center; margin: 1em auto; width: 100%;max-width: 110%;"
 |-
 |[[Image:Review_159642103826-labVirtSpain_20.png|150px|Two degree of freedom satellite]]

@@ Line 521: / Line 521: @@
 [5] L. M. Espinal and F. Silveira Segui, “ La generación de prácticas, proyectos o programas en educación STEM en el marco de una diplomatura virtual para América Latina”, Universidad de Alcalá Servicio de Publicaciones, 2019.
-[6] F. J. Triveño Vargas, http://www.paginasiete.bo/gente/2016/10/27/equipo-bolivianos-desarrolla-algoritmos-para controlar-drones-114891.html, Accessed: 2018-12-12, 2016.
+[6] F. J. Triveño Vargas, https://www.paginasiete.bo/gente/2016/10/27/equipo-bolivianos-desarrolla-algoritmos-para-controlar-drones-114891.html, Accessed: 2018-12-12, 2016.
 [7] F. J. Triveño Vargas,  http://www.lostiempos.com/oh/actualidad/20180312/universidad-no-quieren-dar-paso-adelante, Accessed: 2018-11-11, 2018.

@@ Line 204: / Line 204: @@
 sol = odeint(eqs_mov,state,t,args=(p,))
 </pre>
 |- style="text-align: center; font-size: 75%;"

@@ Line 187: / Line 187: @@
 <pre>
-''from numpy import *
+from numpy import *
 import numpy as np from scipy.integrate
 import odeint import matplotlib.pyplot as plt
@@ Line 202: / Line 202: @@
 p = [g, L, k, u, m]; state = [2., 0]
 t =np.linspace(0,10,300); print (t)
-sol = odeint(eqs_mov,state,t,args=(p,))''
+sol = odeint(eqs_mov,state,t,args=(p,))
 </pre>