Update Content - 2021-09-29
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: [Decoupled Control](decoupled_control.md)
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: [Decoupled Control]({{<relref "decoupled_control.md#" >}})
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Reference
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: ([Chen and McInroy 2004](#org8b1e370))
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: ([Chen and McInroy 2004](#orgbe5d3d7))
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Author(s)
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: Chen, Y., & McInroy, J.
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@@ -20,4 +20,4 @@ Year
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## Bibliography {#bibliography}
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<a id="org8b1e370"></a>Chen, Y., and J.E. McInroy. 2004. “Decoupled Control of Flexure-Jointed Hexapods Using Estimated Joint-Space Mass-Inertia Matrix.” _IEEE Transactions on Control Systems Technology_ 12 (3):413–21. <https://doi.org/10.1109/tcst.2004.824339>.
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<a id="orgbe5d3d7"></a>Chen, Y., and J.E. McInroy. 2004. “Decoupled Control of Flexure-Jointed Hexapods Using Estimated Joint-Space Mass-Inertia Matrix.” _IEEE Transactions on Control Systems Technology_ 12 (3):413–21. <https://doi.org/10.1109/tcst.2004.824339>.
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title = "Simultaneous vibration isolation and pointing control of flexure jointed hexapods"
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author = ["Thomas Dehaeze"]
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draft = false
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Tags
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: [Stewart Platforms]({{< relref "stewart_platforms" >}}), [Vibration Isolation]({{< relref "vibration_isolation" >}})
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Reference
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: ([Li, Hamann, and McInroy 2001](#orgd01725e))
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Author(s)
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: Li, X., Hamann, J. C., & McInroy, J. E.
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Year
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: 2001
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- if the hexapod is designed such that the payload mass/inertia matrix (\\(M\_x\\)) and \\(J^T J\\) are diagonal, the dynamics from \\(u\\) to \\(y\\) are decoupled.
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## Bibliography {#bibliography}
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<a id="orgd01725e"></a>Li, Xiaochun, Jerry C. Hamann, and John E. McInroy. 2001. “Simultaneous Vibration Isolation and Pointing Control of Flexure Jointed Hexapods.” In _Smart Structures and Materials 2001: Smart Structures and Integrated Systems_, nil. <https://doi.org/10.1117/12.436521>.
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content/article/thayer02_six_axis_vibrat_isolat_system.md
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content/article/thayer02_six_axis_vibrat_isolat_system.md
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title = "Six-axis vibration isolation system using soft actuators and multiple sensors"
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author = ["Thomas Dehaeze"]
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draft = true
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Tags
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:
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Reference
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: ([Thayer et al. 2002](#org7584b4b))
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Author(s)
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: Thayer, D., Campbell, M., Vagners, J., & Flotow, A. v.
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Year
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: 2002
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## Bibliography {#bibliography}
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<a id="org7584b4b"></a>Thayer, Doug, Mark Campbell, Juris Vagners, and Andrew von Flotow. 2002. “Six-Axis Vibration Isolation System Using Soft Actuators and Multiple Sensors.” _Journal of Spacecraft and Rockets_ 39 (2):206–12. <https://doi.org/10.2514/2.3821>.
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