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1

Yan, Liang. Design, Modeling and Experiments of 3-DOF Electromagnetic Spherical Actuators. Dordrecht: Springer Science+Business Media B.V., 2011.

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2

Oktay, Baysal y United States. National Aeronautics and Space Administration., eds. 3-D unstructured method for flows past bodies in 6-DOF relative motion: Preprint from proceedings of 6th International Symposium of Computational Fluid Dynamics, Japan Society of Computational Fluid Dynamics, September 4-8, 1995, Lake Tahoe, Nevada. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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3

Oktay, Baysal y United States. National Aeronautics and Space Administration., eds. 3-D unstructured method for flows past bodies in 6-DOF relative motion: Preprint from proceedings of 6th International Symposium of Computational Fluid Dynamics, Japan Society of Computational Fluid Dynamics, September 4-8, 1995, Lake Tahoe, Nevada. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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4

Singh, K. P. 3-D unstructured method for flows past bodies in 6-DOF relative motion: Preprint from proceedings of 6th International Symposium of Computational Fluid Dynamics, Japan Society of Computational Fluid Dynamics, September 4-8, 1995, Lake Tahoe, Nevada. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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5

Oran, Nicks Colby y Langley Research Center, eds. Six degree-of-freedom "live" isolation system tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

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6

Oran, Nicks Colby y Langley Research Center, eds. Six degree-of-freedom "live" isolation system tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

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7

Sahler, Erica. Analysis of a single-degree-of-freedom roll motion model: Simulation, sensitivity study, and comparison to multi-degree-of-freedom models. Springfield, Va: Available from National Technical Information Service, 1996.

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8

Brown, Robert Michael. A microcontroller-based three degree-of-freedom manipulator testbed. [Washington, DC: National Aeronautics and Space Administration, 1995.

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9

Brown, Robert Michael. A microcontroller-based three degree-of-freedom manipulator testbed. [Washington, DC: National Aeronautics and Space Administration, 1995.

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10

Brown, Robert Michael. A microcontroller-based three degree-of-freedom manipulator testbed. [Washington, DC: National Aeronautics and Space Administration, 1995.

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11

Markov, Alexander B. A nonlinear six degree-of-freedom flight simulation model. Ralston, Alta: Defence Research Establishment Suffield, 1990.

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12

Beigie, Darin. Dynamics associated with classical multi-degree-of-freedom scattering phenomena. Ithaca, N.Y: Cornell Theory Center, Cornell University, 1996.

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13

Center, Langley Research, ed. Two degree-of-freedom flutter solution for a personal computer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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14

Center, Langley Research, ed. Two degree-of-freedom flutter solution for a personal computer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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15

Center, Langley Research, ed. Two degree-of-freedom flutter solution for a personal computer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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16

Center, Langley Research, ed. Two degree-of-freedom flutter solution for a personal computer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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17

Williams, Robert L. Kinematics of the six-degree-of-freedom force-reflecting Kraft Master. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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18

United States. National Aeronautics and Space Administration., ed. Research related to multi degree of freedom magnetic suspensions: A thesis ... [Washington, DC: National Aeronautics and Space Administration, 1997.

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19

Goldfarb, Michael. Design of a minimum surface-effect three degree-of-freedom micromanipulator. [Washington, DC: National Aeronautics and Space Administration, 1997.

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20

Williams, Robert L. Kinematics of the six-degree-of-freedom force-reflecting Kraft Master. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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21

United States. National Aeronautics and Space Administration., ed. Research related to multi degree of freedom magnetic suspensions: A thesis ... [Washington, DC: National Aeronautics and Space Administration, 1997.

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22

Williams, Robert L. Kinematics of the six-degree-of-freedom force-reflecting Kraft Master. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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23

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. The effect of acceleration versus displacement methods on steady-state boundary forces. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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24

M, Eisenberg Judah, ed. Quantum mechanics of many degrees of freedom. New York: Wiley, 1988.

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25

Linear vibrations: A theoretical treatment of multi-degree-of-freedom vibrating systems. Dordrecht: Nijhoff, 1985.

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26

Ebeling, Robert M. Accuracy of response of single-degree-of-freedom systems to ground motion. Vicksburg, Miss: U.S. Army Engineer Waterways Experiment Station, 1997.

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27

A, Troutman Patrick y Langley Research Center, eds. Space Station Freedom assembly and operation at a 51.6 degree inclination orbit. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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28

United States. National Aeronautics and Space Administration., ed. Dynamics and control of a five degree-of-freedom magnetic suspension system. Norfolk, Va: Old Dominion University Research Foundation, 1992.

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29

Müller, P. C. Linear vibrations: A theoretical treatment of multi-degree-of-freedom vibrating systems. Dordrecht: Springer Netherlands, 1985.

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30

Williams, Robert L. Local performance optimization for a class of redundant eight-degree-of-freedom manipulators. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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31

Hu, Paul Xue Bang. Development of a paediatric prosthetic hand with a two-degree-of-freedom thumb. Ottawa: National Library of Canada, 1997.

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32

Reed, Stephen Charles. The clinical application of a 6-degree of freedom electrogoniometer (instrumented spatial linkage device). Ottawa: National Library of Canada, 1990.

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33

Center, Langley Research, ed. Simplified analytical model of a six-degree-of-freedom large-gap magnetic suspension system. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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34

Institute, American National Standards y IEEE Aerospace and Electronic Systems Society. Gyro and Accelerometer Panel., eds. IEEE specification format guide and test procedure for two-degree-of-freedom dynamically tuned gyros. New York, NY, USA: Institute of Electrical and Electronics Engineers, 1989.

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35

Williams, Robert L. Kinematic equations for control of the redundant eight-degree-of-freedom advanced research manipulator II. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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36

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Kinematic equations for control of the redundant eight-degree-of-freedom advanced research manipulator II. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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37

Potter, Scott Alton. Full pose and partial pose calibration of a six degree of freedom robot manipulator arm. Monterey, Calif: Naval Postgraduate School, 1991.

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38

Goodrich, Kenneth H. A high-fidelity, six-degree-of-freedom batch simulation environment for tactical guidance research and evaluation. Hampton, Va: Langley Research Center, 1993.

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39

Center, Ames Research, ed. An aerodynamic model for one and two degree of freedom wing rock of slender delta wings. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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40

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, ed. A high-fidelity, six-degree-of-freedom batch simulation environment for tactical guidance research and evaluation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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41

The degree of our commitment to our national motto "freedom and justice" since independence: An assessment. Ghana]: [publisher not identified], 2007.

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42

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. A high-fidelity, six-degree-of-freedom batch simulation environment for tactical guidance research and evaluation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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43

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. A high-fidelity, six-degree-of-freedom batch simulation environment for tactical guidance research and evaluation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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44

Ph, Chomaz, ed. Dynamics and thermodynamics with nuclear degrees of freedom. Berlin: SIF, Springer, 2006.

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45

Ph, Chomaz, ed. Dynamics and thermodynamics with nuclear degrees of freedom. Berlin: SIF, Springer, 2006.

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46

Yan, Liang, Guilin Yang, Kok-Meng Lee, I.-Ming Chen y Chee Kian Lim. Design, Modeling and Experiments of 3-DOF Electromagnetic Spherical Actuators. Springer, 2016.

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47

Vaicis, Ivo. Shape Optimization of Mechanical System Elements Considering Uncertainty. RTU Press, 2022. http://dx.doi.org/10.7250/9789934227356.

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In the Thesis a new method is developed for optimising the shape of mechanical elements by considering the interaction of these elements with a multiphase uncertainty environment whose approximation model achieves a significant number of degrees of freedom (DOF). The Thesis analyses the process of dust formation during the handling of granular material. Different experimental designs are used to derive metamodels and to analyse the segregation of granular material in the silo discharge depending on the oscillation frequency, amplitude, and geometrical characteristics of the silo.
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48

Lorna, Tedder. Third Degree of Freedom. Spilled Candy Publications, 2006.

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49

One Degree of Freedom. Illuminate YA, 2020.

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50

Sturt, A. C. A Degree of Freedom. Churinga Publishing, 1995.

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