Update all files with new citeproc-org package

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: [HAC-HAC]({{< relref "hac_hac" >}})
Reference
: <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>
: ([Bryson 1993](#orgcd1f1a3))
Author(s)
: Bryson, A. E.
@@ -41,11 +41,13 @@ Year
> LAC uses a co-located rate sensor to add damping to all the vibratory modes (but not the rigid-body mode).
> 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")
<a id="orgdde3e8f"></a>
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{{< figure src="/ox-hugo/bryson93_hac_lac.png" caption="Figure 1: HAC-LAC control concept" >}}
> 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.
# Bibliography
<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)
## Bibliography {#bibliography}
<a id="orgcd1f1a3"></a>Bryson, Arthur Earl. 1993. _Control of Spacecraft and Aircraft_. Princeton university press Princeton, New Jersey.