1. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Flight simulator motion system Figure Legend:

2. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 The UPS Stewart platform Figure Legend:

3. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Posicion analysis of one leg Figure Legend:

4. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Z-Y-X Euler angles Figure Legend:

5. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Velocity analysis of one leg Figure Legend:

6. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Axes of the universal joint Figure Legend:

7. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Acceleration analysis of one leg Figure Legend:

8. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Frames of references of one leg Figure Legend:

9. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Dynamic analysis of one leg Figure Legend:

10. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Dynamic analysis of the platform Figure Legend:

11. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Representation of the electromechanical servo-actuator Figure Legend:

12. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Inverse dynamic Figure Legend:

13. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Rejected take-off maneuver: (a) acceleration components and (b) angular velocity components Figure Legend:

14. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Desired motion simulator-position: (a) linear position components and (b) Euler angles Figure Legend:

15. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Desired motion simulator-acceleration: (a) acceleration components and (b) Euler angles rates Figure Legend:

16. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Driving torques supplied by the servomotors Figure Legend:

17. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Motor angular velocities Figure Legend:

18. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Driving forces supplied by the actuators Figure Legend:

19. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Errors caused by simplification of leg acceleration Figure Legend:

20. Date of download: 9/19/2016 Copyright © ASME. All rights reserved. From: Dynamic Modeling of a Six Degree-of-Freedom Flight Simulator Motion Base J. Comput. Nonlinear Dynam. 2015;10(5):051020-051020-13. doi:10.1115/1.4030013 Platform and base leg points distribution Figure Legend: