Update all files with new citeproc-org package
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@@ -8,7 +8,7 @@ Tags
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: [HAC-HAC]({{< relref "hac_hac" >}})
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Reference
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: <sup id="4970865a21830fff7b1daeec187bfa68"><a class="reference-link" href="#bryson93_contr_spacec_aircr" title="Bryson, Control of Spacecraft and Aircraft, Princeton university press Princeton, New Jersey (1993).">(Bryson, 1993)</a></sup>
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: ([Bryson 1993](#orgcd1f1a3))
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Author(s)
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: Bryson, A. E.
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@@ -41,11 +41,13 @@ Year
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> LAC uses a co-located rate sensor to add damping to all the vibratory modes (but not the rigid-body mode).
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> HAC uses a separated displacement sensor to stabilize the rigid body mode, which slightly decreases the damping of the vibratory modes but not enough to produce instability (called "spillover")
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<a id="orgdde3e8f"></a>
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<a id="org3548362"></a>
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{{< figure src="/ox-hugo/bryson93_hac_lac.png" caption="Figure 1: HAC-LAC control concept" >}}
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> LAC/HAC is usually insensitive to small deviation of the plant dynamics away from the design values, that is, it is **robust** to plant parameter changes.
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# Bibliography
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<a class="bibtex-entry" id="bryson93_contr_spacec_aircr">Bryson, A. E., *Control of spacecraft and aircraft* (1993), : Princeton university press Princeton, New Jersey.</a> [↩](#4970865a21830fff7b1daeec187bfa68)
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## Bibliography {#bibliography}
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<a id="orgcd1f1a3"></a>Bryson, Arthur Earl. 1993. _Control of Spacecraft and Aircraft_. Princeton university press Princeton, New Jersey.
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