diff --git a/src/pages/about/docs.astro b/src/pages/about/docs.astro
index 4bf40d925..92a52c2ee 100644
--- a/src/pages/about/docs.astro
+++ b/src/pages/about/docs.astro
@@ -844,6 +844,38 @@ All titles should be done in sentence case.
 
 </SubSubSection> 
 
+<SubSubSection title = "Links to Warnings" id = "links_to_warnings">
+    <p>
+        Tag type: Warning
+    </p>
+    Options:
+    <ul>
+        <li>href: insert the id of the warning you want to link to after '#warning_'.</li>
+    </ul>
+    Example:
+    <CodeBox language = "html" code = `<a href = "/xxx/CoursePage#warning_id">TEXT</a>`/>
+    <a href = "/dyn/vectors#warning_rvv-wl">TEXT</a>
+    <p>
+        <em>*For demonstration purposes, this links to a warning in the vectors page in dynamics.</em>
+    </p>
+</SubSubSection>
+
+<SubSubSection title = "Links to Examples" id = "links_to_examples">
+    <p>
+        Tag type: Example
+    </p>
+    Options:
+    <ul>
+        <li>href: insert the id of the example you want to link to after '#example_btn_'.</li>
+    </ul>
+    Example:
+    <CodeBox language = "html" code = `<a href = "/xxx/CoursePage#example_btn_id">TEXT</a>`/>
+    <a href = "/dyn/vectors#example_btn_rvv-xn">TEXT</a>
+    <p>
+        <em>*For demonstration purposes, this links to an example in the vectors page in dynamics.</em>
+    </p>
+</SubSubSection>
+
 <SubSubSection title="External page" id="ext-page">
 
     <p>Tag type: Regular</p>
diff --git a/src/pages/dyn/contact_and_rolling.astro b/src/pages/dyn/contact_and_rolling.astro
index 3f20f7dd9..ea99d74bb 100644
--- a/src/pages/dyn/contact_and_rolling.astro
+++ b/src/pages/dyn/contact_and_rolling.astro
@@ -190,11 +190,11 @@ import CalloutContainer from "../../components/CalloutContainer.astro"
     <DisplayEquation equation="\\begin{aligned}            \\vec{v}_C &amp;= r \\omega \\,\\hat{e}_t \\\\            \\vec{a}_C &amp;= r \\alpha \\,\\hat{e}_t            \\end{aligned}" background="True" title="Center velocity and acceleration while rolling on a flat surface (Tangential-Normal Basis)." id="rko-ef" derivation="True">
         <p>
             We begin by observing that the sign conventions in
-            Figure <a href="#rko-ff">#rko-ff</a> mean that
+            Figure <a href="#rolling_flat_surface">#rko-ff</a> mean that
             <InlineEquation equation="\\vec\\omega = -\\omega\\,\\hat{e}_b" />. Now rolling without
             slipping means the contact point \(A\) must
             instantaneously have zero velocity, so using <a
-            href="rkg.html#rkg-er">#rkg-er</a> gives:
+            href="/dyn/rigid_body_kinematics#rkg-er">#rkg-er</a> gives:
 
             <DisplayEquation equation="\\begin{aligned}            \\vec{v}_C &amp;= \\vec{v}_A + \\vec{\\omega} \\times \\vec{r}_{AC} \\\\            &amp;= (-\\omega \\,\\hat{e}_b) \\times r \\,\\hat{e}_n \\\\            &amp;= r \\omega \\,\\hat{e}_t.            \\end{aligned}" />
 
@@ -247,7 +247,7 @@ import CalloutContainer from "../../components/CalloutContainer.astro"
                 By definition of non-slip rolling contact, the point of
                 contact \(P\) has zero velocity. The acceleration can be
                 computed from the center \(C\) with <a
-                href="#rkg-e2">#rkg-e2</a>:
+                href="/dyn/rigid_body_kinematics#rkg-e2">#rkg-e2</a>:
     
                 <DisplayEquation equation="\\begin{aligned}            \\vec{a}_P &amp;= \\vec{a}_C + \\vec{\\alpha} \\times \\vec{r}_{CP}            + \\vec{\\omega} \\times (\\vec{\\omega} \\times \\vec{r}_{CP}) \\\\            &amp;= \\alpha r \\,\\hat{e}_t + (-\\alpha\\,\\hat{e}_b) \\times (-r\\,\\hat{e}_n)            + (-\\omega\\,\\hat{e}_b) \\times \\Big((-\\omega\\,\\hat{e}_b) \\times (-r\\,\\hat{e}_n)\\Big) \\\\            &amp;= \\alpha r \\,\\hat{e}_t - \\alpha r \\,\\hat{e}_t            + \\omega^2 r \\,\\hat{e}_n \\\\            &amp;= \\omega^2 \\,\\vec{r}_{PC}.            \\end{aligned}"/>
               </p>
diff --git a/src/pages/dyn/geometric_properties.astro b/src/pages/dyn/geometric_properties.astro
index 3222209d6..6d370e578 100644
--- a/src/pages/dyn/geometric_properties.astro
+++ b/src/pages/dyn/geometric_properties.astro
@@ -105,7 +105,7 @@ import Row from "../../components/Row.astro"
                 <DisplayEquation equation="\\vec{r}_C = \\frac{1}{m}\\iiint_{\\mathcal{B}} \\vec{r} dm" />
             </p>
             <p>
-                Where <InlineEquation equation="dm = \\rho \\, dV" /> from the differential of <a href="rcm.html#rcm-tm">#rcm-tm</a>. Substituting in:
+                Where <InlineEquation equation="dm = \\rho \\, dV" /> from the differential of <a href="/dyn/geometric_properties#rcm-tm">#rcm-tm</a>. Substituting in:
                 <DisplayEquation equation="\\begin{aligned} \\vec{r}_C &amp;= \\frac{1}{m}\\iiint_{\\mathcal{B}} \\vec{r} dm \\\\ &amp;= \\frac{1}{m}\\iiint_{\\mathcal{B}} \\vec{r} \\rho \\, dV \\\\ &amp;= \\frac{1}{m}\\iiint_{\\mathcal{B}} \\rho \\vec{r} \\, dV \\\\ \\end{aligned}" />
             </p>
         </div>
@@ -361,8 +361,8 @@ import Row from "../../components/Row.astro"
                 <DisplayEquation equation="\\begin{aligned} x_C &amp;= \\frac{\\rho}{m}\\int_{0}^{1}\\int_{0}^{1 - u} (x_P u + x_Q v) \\, J \\, dvdu \\\\ &amp;= \\frac{\\rho}{m}\\int_{0}^{1}\\int_{0}^{1 - u} (x_P u + x_Q v) \\, (x_P y_Q - x_Q y_P) \\, dvdu \\\\ &amp;= \\frac{\\rho}{m}(x_P y_Q - x_Q y_P)\\int_{0}^{1}\\int_{0}^{1 - u} (x_P u + x_Q v) \\, dvdu \\\\ &amp;= \\frac{\\rho}{m}(x_P y_Q - x_Q y_P)\\int_{0}^{1}x_P u\\left[v\\right]_{v = 0}^{v = 1-u} + \\frac{x_Q}{2}\\left[v^2\\right]_{v = 0}^{v = 1-u}du \\\\ &amp;= \\frac{\\rho}{m}(x_P y_Q - x_Q y_P)\\int_{0}^{1} x_P u(1 - u) + \\frac{x_Q}{2}(1 - u)^2 du \\\\ &amp;= \\frac{\\rho}{m}(x_P y_Q - x_Q y_P) \\left(\\frac{x_P}{2} \\left[u^2\\right]_{0}^{1} - \\frac{x_P}{3}\\left[u^3\\right]_{0}^{1}  + \\frac{x_Q}{2}\\left[u\\right]_{0}^{1} - \\frac{x_Q}{2}\\left[u^2\\right]_{0}^{1} + \\frac{x_Q}{6}\\left[u^3\\right]_{0}^{1}\\right) \\\\  &amp;= \\frac{\\rho}{m}(x_P y_Q - x_Q y_P) \\left(\\frac{x_P}{2} - \\frac{x_P}{3} + \\frac{x_Q}{2} - \\frac{x_Q}{2} + \\frac{x_Q}{6}\\right) \\\\ &amp;= \\frac{\\rho}{m}(x_P y_Q - x_Q y_P) \\left(\\frac{x_P + x_Q}{6}\\right) \\end{aligned}" />
             </p>
             <p>
-                The total mass of the plate is <InlineEquation equation="m = \rho A = \frac{1}{2}\rho x_P y_Q" />, and with the chosen configuration \(y_P = 0\). Thus:
-                <DisplayEquation equation="x_C = \frac{x_P + x_Q}{3}" />
+                The total mass of the plate is <InlineEquation equation="m = \\rho A = \\frac{1}{2}\\rho x_P y_Q" />, and with the chosen configuration \(y_P = 0\). Thus:
+                <DisplayEquation equation="x_C = \\frac{x_P + x_Q}{3}" />
             </p>
         </div>
     </DisplayEquationCustom>
@@ -383,7 +383,7 @@ import Row from "../../components/Row.astro"
                 <DisplayEquation equation="\\begin{aligned} \\vec{r}_C &amp;= \\frac{1}{m}\\iiint_\\mathcal{B} \\rho \\vec{r} \\, dV \\\\ &amp;= \\frac{1}{m}\\iint_{A} \\rho \\vec{r} \\, dA \\\\ \\end{aligned}" />
             </p>
             <p>
-                It is convenient to switch to <a href="rvy.html#rvy-ec">cylindrical coordinates</a>: 
+                It is convenient to switch to <a href="/dyn/coordinate_systems#cylindrical_coordinates">cylindrical coordinates</a>: 
                 <DisplayEquation equation="\\begin{aligned} x &amp;= a \\, r \\cos\\theta \\\\ y &amp;= b \\, r \\sin\\theta \\\\ \\end{aligned}" />
             </p>
             <p>
@@ -404,7 +404,7 @@ import Row from "../../components/Row.astro"
 
 <SubSubSection title="Simplified shapes" id="simple_shapes_com">
     <p>
-        The centers of mass listed below are all special cases of the basic shapes given in Section <a href="#rcm-bs">#rcm-bs</a>. Other
+        The centers of mass listed below are all special cases of the basic shapes given in Section <a href="/dyn/geometric_properties#basic_shapes_com">#rcm-bs</a>. Other
         special cases can be easily obtained by similar methods, or directly computing the integral.
     </p>
     
@@ -421,7 +421,7 @@ import Row from "../../components/Row.astro"
 
         <div slot="derivation">
             <p>
-                See <a href="#rcm-xc">example problem</a> on how to derive it by directly computing the integrals.
+                See <a href="/dyn/geometric_properties#example_btn_rcm-xc">example problem</a> on how to derive it by directly computing the integrals.
             </p>
             <p>
                 The other perhaps simpler approach is to let \(x_Q = 0\) in <a href="#rcm-et">#rcm-et</a>, which forms a right triangle if the configuration
@@ -444,7 +444,7 @@ import Row from "../../components/Row.astro"
 
         <div slot="derivation">
             <p>
-                See <a href="#rcm-xc">example problem</a> on how to derive it by directly computing the integrals.
+                See <a href="/dyn/geometric_properties#example_btn_rcm-xc">example problem</a> on how to derive it by directly computing the integrals.
             </p>
             <p>
                 The other perhaps simpler approach is to let \(x_Q = 0\) in <a href="#rcm-et">#rcm-et</a>, which forms a right triangle if the configuration
@@ -473,7 +473,7 @@ import Row from "../../components/Row.astro"
                 <DisplayEquation equation="\\begin{aligned} \\vec{r}_C &amp;= \\frac{1}{m}\\iiint_\\mathcal{B} \\rho \\vec{r} \\, dV \\\\ &amp;= \\frac{1}{m}\\iint_{A} \\rho \\vec{r} \\, dA \\\\ \\end{aligned}" />
             </p>
             <p>
-                It is convenient to switch to <a href="rvy.html#rvy-ec">cylindrical coordinates</a>:
+                It is convenient to switch to <a href="/dyn/coordinate_systems#cylindrical_coordinates">cylindrical coordinates</a>:
                 <DisplayEquation equation="\\begin{aligned} x &amp;= r \\cos\\theta \\\\ y &amp;= r \\sin\\theta \\\\ \\end{aligned}"/>
             </p>
             <p>
@@ -823,7 +823,7 @@ import Row from "../../components/Row.astro"
 
                   <p>
                     Use the answer to Example Problem <a
-                    href="#rem-xs">#rem-xs</a> and the parallel axis
+                    href="#example_btn_rem-xs">#rem-xs</a> and the parallel axis
                     theorem <a href="#rem-el">#rem-el</a>.
                   </p>
             </div>
@@ -834,7 +834,7 @@ import Row from "../../components/Row.astro"
 
         <div slot="solution">
             <p>
-                In Example Problem <a href="#rem-xs">#rem-xs</a> we
+                In Example Problem <a href="#example_btn_rem-xs">#rem-xs</a> we
                 computed the moment of inertia of a square place
                 about the center to be <InlineEquation equation="I_{C,z} = \\frac{1}{6} m \\ell^2" />. The parallel axis theorem <a
                 href="#rem-el">#rem-el</a> now gives:
@@ -963,7 +963,7 @@ import Row from "../../components/Row.astro"
                 <div class="w-50">
                     <p>
                         Recall that in Example Problem <a
-                        href="#rem-xs">#rem-xs</a> we computed the
+                        href="#example_btn_rem-xs">#rem-xs</a> we computed the
                         moment of inertia of a square place about the center
                         to be <InlineEquation equation="I_{C,z} = \\frac{1}{6} m \\ell^2" />.
                       </p>
@@ -1077,7 +1077,7 @@ import Row from "../../components/Row.astro"
             <p>
                 To compute the integrals in <a
                 href="#rem-ec">#rem-ec</a> it is convenient to switch to
-                <a href="rvy.html">cylindrical coordinates</a>:
+                <a href="/dyn/coordinate_systems#cylindrical_coordinates">cylindrical coordinates</a>:
             </p>
             <DisplayEquation equation="\\begin{aligned}x &= r \\cos\\theta \\\\y &= r \\sin\\theta \\\\z &= z.\\end{aligned}\\" /> 
 
@@ -1131,7 +1131,7 @@ import Row from "../../components/Row.astro"
         <p>
             To compute the integrals in <a
             href="#rem-ec">#rem-ec</a> it is convenient to switch to
-            <a href="rvs.html">spherical coordinates</a>:
+            <a href="/dyn/coordinate_systems#spherical_coordinates">spherical coordinates</a>:
         </p>
         <DisplayEquation equation="\\begin{aligned}x &= r \\cos\\theta \\sin\\phi \\\\y &= r \\sin\\theta \\sin\\phi \\\\z &= r \\cos\\phi.\\end{aligned}\\" /> 
 
@@ -1160,7 +1160,7 @@ import Row from "../../components/Row.astro"
     <p>
         The moments of inertia listed below are all special cases of
         the basic shapes given in Section <a
-        href="#rem-sb">#rem-sb</a>. Other special cases can be
+        href="#basic_shapes_moi">#rem-sb</a>. Other special cases can be
         easily obtained by similar methods.
       </p>
 
diff --git a/src/pages/dyn/momentum.astro b/src/pages/dyn/momentum.astro
index e6533c41a..d2928001a 100644
--- a/src/pages/dyn/momentum.astro
+++ b/src/pages/dyn/momentum.astro
@@ -255,7 +255,7 @@ import Col from "../../components/Col.astro"
 		</p>
 		<p>
 			The cross product of a vector with itself is zero 
-			(<a href="rvi.html#rvi-ez">cross product self-annihilation</a>). So the
+			(<a href="/dyn/vector_calculus#rvi-ez">cross product self-annihilation</a>). So the
 			integral of <InlineEquation equation="\\int m\\vec{v}_P \\times \\vec{v}_P \\, dt" />			is a constant, which is 
 			the initial angular momentum. Assuming this is zero, we arrive at the 
 			desired expression.
@@ -299,7 +299,7 @@ import Col from "../../components/Col.astro"
 
 	<Example title="The Rocket Equation" id="rec-xr" solution="false">
 		<p>
-			As stated in the warning at <a href="#rec-wm">#rec-wm</a>, the 
+			As stated in the warning at <a href="#warning_rec-wm">#rec-wm</a>, the 
 			relationship between Newton's equations and linear momentum are 
 			not applicable for a system whose mass is changing with time. To use
 			that relationship, a few things must be changed. Consider the figure 
diff --git a/src/pages/dyn/particle_kinematics.astro b/src/pages/dyn/particle_kinematics.astro
index 56a526430..34cbd2d15 100644
--- a/src/pages/dyn/particle_kinematics.astro
+++ b/src/pages/dyn/particle_kinematics.astro
@@ -198,7 +198,7 @@ import InlineCanvas from "../../components/InlineCanvas.astro"
       </table>
       <p class="figureCaption mt-2">
         Velocity and acceleration of various movements. Compare to
-        Figure <a href="rvc.html#rvc-fp">#rvc-fp</a>.
+        Figure <a href="/dyn/vector_calculus#derivatives_and_vector_positions">#rvc-fp</a>.
       </p>
      </PrairieDrawCanvas>
 		 
@@ -551,7 +551,7 @@ import InlineCanvas from "../../components/InlineCanvas.astro"
             Take <InlineEquation equation="\\hat{a}" /> to be a unit vector rotating in the 2D
             <InlineEquation equation="\\hat\\imath–\\hat\\jmath" /> plane, making an angle of
             \(\theta\) with the \(x\)-axis, as in Figure <a
-            href="#rkr-f2">#rkr-f2</a>. Then:
+            href="#rkr-fe-c">#rkr-fe-c</a>. Then:
 
             <DisplayEquation equation="\\hat{a} = \\cos\\theta \\,\\hat\\imath            + \\sin\\theta \\,\\hat\\jmath." />
 
diff --git a/src/pages/dyn/rigid_body_kinematics.astro b/src/pages/dyn/rigid_body_kinematics.astro
index 4f74c8c7f..0bbd60af7 100644
--- a/src/pages/dyn/rigid_body_kinematics.astro
+++ b/src/pages/dyn/rigid_body_kinematics.astro
@@ -229,7 +229,7 @@ import DisplayTable from "../../components/DisplayTable.astro"
                 <DisplayEquation equation="\\begin{aligned}  \\vec{r}_Q &amp;= \\vec{r}_P + \\vec{r}_{PQ} \\\\  \\dot{\\vec{r}}_Q &amp;= \\dot{\\vec{r}}_P  + \\dot{\\vec{r}}_{PQ} \\\\  \\vec{v}_Q &amp;= \\vec{v}_P  + \\vec{\\omega} \\times \\vec{r}_{PQ},  \\end{aligned}" />
   
                 where the derivative of <InlineEquation equation="\\vec{r}_{PQ}" /> comes from the <a
-                href="rkr.html#rkr-ew">rotation formula</a>, given that
+                href="/dyn/particle_kinematics/#rkr-ew">rotation formula</a>, given that
                 this offset vector is simply rotating with the rigid
                 body.
               </p>
@@ -246,7 +246,7 @@ import DisplayTable from "../../components/DisplayTable.astro"
     <Warning id="rkg-wc" title="Cross product order">
         <p>
             Because cross products are <a
-            href="/dyn/vector_calculus#rvv-wc">not associative</a>, it is very
+            href="/dyn/vector_calculus#warning_rvv-wc">not associative</a>, it is very
             important to compute the centripetal acceleration term
             with the parentheses as shown. That is, we must not
             compute <InlineEquation equation="(\\vec{\\omega} \\times \\vec{\\omega}) \\times \\vec{r}_{PQ}" />, as this is always zero.
@@ -415,7 +415,7 @@ import DisplayTable from "../../components/DisplayTable.astro"
   
                 Evaluating <a href="#rkg-er">#rkg-er</a> and using the
                 cross-product expression <a
-                href="rvv.html#rvv-e9">#rvv-e9</a> now gives the
+                href="/dyn/vector_calculus#rvv-e9">#rvv-e9</a> now gives the
                 velocity expression:
   
                 <DisplayEquation equation="\\begin{aligned}  \\vec{v}_Q &amp;= \\vec{v}_P  + \\vec{\\omega} \\times \\vec{r}_{PQ} \\\\  &amp;= \\vec{v}_P  + \\omega\\,\\hat{k} \\times \\vec{r}_{PQ} \\\\  &amp;= \\vec{v}_P  + \\omega \\,\\vec{r}_{PQ}^\\perp,  \\end{aligned}" />
@@ -937,13 +937,13 @@ import DisplayTable from "../../components/DisplayTable.astro"
         We can use conservation of energy to obtain an expression for <InlineEquation equation="\\dot\\theta" />.  
     </p>
     <p>
-        Using <a href="#">the work-energy theorem</a>:
+        Using <a href="/dyn/work_and_energy#ren-eco">the work-energy theorem</a>:
         <DisplayEquation equation="        W = \\Delta T + \\Delta V        " />
 
     </p>
     <p>
         The rod is sliding along frictionless surfaces, so there are no non-conservative forces present,
-        and constraint forces do no work (See <a href="#">work done by a constraint force</a>)
+        and constraint forces do no work (See <a href="/dyn/work_and_energy#ren-wt">work done by a constraint force</a>)
     </p>
     <p>
         Therefore:
@@ -1014,7 +1014,7 @@ import DisplayTable from "../../components/DisplayTable.astro"
 
   <div slot="solution">
     <p>
-      We added one more assumption to the ones made in <a href="#rkc-xcp">#rkc-xcp</a>. Namely, the rope can only slip.
+      We added one more assumption to the ones made in <a href="#example_btn_rkc-xcp">#rkc-xcp</a>. Namely, the rope can only slip.
       This simply means that the tension is the same at any point in the rope.
   </p>
   <p>
@@ -1052,7 +1052,7 @@ import DisplayTable from "../../components/DisplayTable.astro"
       <DisplayEquation equation="            T - m_2 g = m_2 a_2      " />
   </p>
   <p>
-      We have 3 unknowns, 2 equations. We apply our constraint equation from <a href="#rkc-xcp">#rkc-xcp</a> to relate
+      We have 3 unknowns, 2 equations. We apply our constraint equation from <a href="#example_btn_rkc-xcp">#rkc-xcp</a> to relate
       the accelerations of <InlineEquation equation="m_1" /> and <InlineEquation equation="m_2" />:
       <DisplayEquation equation="      2a_1 + a_2 = 0      " />
 
diff --git a/src/pages/dyn/steering_geometry.astro b/src/pages/dyn/steering_geometry.astro
index 48b7b2313..9f76d1219 100644
--- a/src/pages/dyn/steering_geometry.astro
+++ b/src/pages/dyn/steering_geometry.astro
@@ -68,8 +68,10 @@ import DisplayTable from "../../components/DisplayTable.astro"
 
     <CalloutContainer slot="cards">
       <CalloutCard title="Reference material">
-        <li><a href = "/dyn/rigid_body_kinematics#rigid_bodies">Rigid bodies</a></li>
-        <li><a href = "/dyn/rigid_body_kinematics#constrained_motion">Constrained motion</a></li>
+        <ul>
+          <li><a href = "/dyn/rigid_body_kinematics#rigid_bodies">Rigid bodies</a></li>
+          <li><a href = "/dyn/rigid_body_kinematics#constrained_motion">Constrained motion</a></li>
+        </ul>
       </CalloutCard>
     </CalloutContainer>
 </Section>
diff --git a/src/pages/dyn/work_and_energy.astro b/src/pages/dyn/work_and_energy.astro
index 030119f0d..ecd241d22 100644
--- a/src/pages/dyn/work_and_energy.astro
+++ b/src/pages/dyn/work_and_energy.astro
@@ -59,7 +59,7 @@ import Col from "../../components/Col.astro"
 
 <DisplayEquation equation="\\begin{aligned}\\vec{F} &amp;= -\\nabla V \\\\&amp; = -\\frac{\\partial V}{\\partial x}\\hat{\\imath} -\\frac{\\partial V}{\\partial y}\\hat{\\jmath} - \\frac{\\partial V}{\\partial z}\\hat{k}\\end{aligned}" id="ren-efp" title="Force and potential energy." background="True" derivation="True">
 	<p>
-		Beginning with <a href="#ren-ec">#ren-ec</a> and generalizing it to one-dimensional displacement in the y-direction, the equation becomes:
+		Beginning with <a href="#ren-wc">#ren-wc</a> and generalizing it to one-dimensional displacement in the y-direction, the equation becomes:
 		<DisplayEquation equation="\\begin{aligned}		W &amp;= \\vec{F} \\cdot \\Delta{\\vec{y}}		\\end{aligned}" />
 
 	</p>
@@ -105,7 +105,7 @@ import Col from "../../components/Col.astro"
 
 		  </p>
 		  <p>
-			Since gravity only acts in one direction, we can simplify <a href="ren-efp">#ren-efp</a> to:
+			Since gravity only acts in one direction, we can simplify <a href="/dyn/work_and_energy#ren-efp">#ren-efp</a> to:
 			<DisplayEquation equation="\\begin{aligned}			F &amp;= -\\frac{dV}{dy} \\\\			-mg &amp;= -\\frac{dV}{dy} \\\\			mg \\, dy &amp;= dV \\\\			\\end{aligned}" />
 
 		  </p>
@@ -141,7 +141,7 @@ import Col from "../../components/Col.astro"
 
 		  </p>
 		  <p>
-			Since the restoring force in a spring only acts in one direction, we can simplify <a href="ren-efp">#ren-efp</a> to:
+			Since the restoring force in a spring only acts in one direction, we can simplify <a href="/dyn/work_and_energy#ren-efp">#ren-efp</a> to:
 			<DisplayEquation equation="\\begin{aligned}			F &amp;= -\\frac{dV}{dx} \\\\			-kx &amp;= -\\frac{dV}{dx} \\\\			kx \\, dx &amp;= dV \\\\			\\end{aligned}" />
 
 		  </p>
@@ -238,7 +238,7 @@ import Col from "../../components/Col.astro"
 
 	</p>
 	<p>
-		Using conservation of energy, and the fact that a vector dotted with itself equals its magnitude squared (see <a href="rvi.html#rvi-eg">#rvi-eg</a>), then:
+		Using conservation of energy, and the fact that a vector dotted with itself equals its magnitude squared (see <a href="/dyn/vector_calculus#rvi-eg">#rvi-eg</a>), then:
 		<DisplayEquation equation="\\begin{aligned}		T &amp; = \\frac{1}{2}mv^2\\\\		\\end{aligned}" />
 
 	</p>
@@ -290,14 +290,14 @@ import Col from "../../components/Col.astro"
 
 <DisplayEquation id="ren-ea" equation="T = \\frac{1}{2} m v_Q^2 + m \\vec{v}_Q \\cdot \\left( \\vec\\omega \\times \\vec{r}_{QC} \\right) + \\frac{1}{2} I_{Q,\\hat\\omega} \\omega^2" title="Kinetic energy of a rigid body about an arbitrary body point \\(Q\\)." background="True" derivation="true">
 	<p>
-		We start with the general expression <a href="#rem-eb">#rem-eb</a>:
+		We start with the general expression <a href="/dyn/geometric_properties#rem-eb">#rem-eb</a>:
 
 		<DisplayEquation equation="\\begin{aligned}		T &amp;= \\iiint_{\\mathcal{B}} \\frac{1}{2} \\rho v_P^2 \\, dV,		\\end{aligned}" />
 
 
 		where we integrate over the body with a location \(P\). We
 		choose a point \(Q\) fixed to the body and
-		use <a href="rkg.html#rkg-er">#rkg-er</a> to express the
+		use <a href="/dyn/rigid_body_kinematics#rkg-er">#rkg-er</a> to express the
 		velocity of \(P\) in terms of <InlineEquation equation="\\vec{v}_Q" /> and
 		\(\vec\omega\), giving
 
@@ -317,7 +317,7 @@ import Col from "../../components/Col.astro"
 		orthogonal distance to point \(P\) from the line through
 		\(Q\) in direction <InlineEquation equation="\\vec\\omega" />
 		, so
-		from <a href="rem.html#rem-ei">#rem-ei</a> we see that
+		from <a href="/dyn/geometric_properties#rem-ei">#rem-ei</a> we see that
 		the final integral above is the moment of inertia
 		<InlineEquation equation="I_{Q,\\hat\\omega}" />
   about the  axis through
@@ -333,7 +333,7 @@ import Col from "../../components/Col.astro"
 </DisplayEquation>
 
 <DisplayEquationCustom id="ren-eco" title="Work-energy theorem." background="True">
-	<DisplayEquation equation="W = \Delta T + \Delta V"/>
+	<DisplayEquation equation="W = \\Delta T + \\Delta V"/>
 	<p>
 		where \(W\) is the work done by non-conservative forces. If non-conservative forces are not present, then
 		it becomes conservation of energy.
@@ -405,7 +405,7 @@ import Col from "../../components/Col.astro"
 		</div>
 	</DisplayEquationCustom>
 
-	<DisplayEquationCustom id="ren-wm" title="Work done by a moment \\(M\\)." background="True" derivation="true">
+	<DisplayEquationCustom id="ren-wm" title="Work done by a moment \\(M\\)." background="True">
 		<DisplayEquation equation="\\begin{aligned}W &amp;= \\int_{\\theta_1}^{\\theta_2} M \\, d\\theta \\\\&amp; = \\int_{t_1}^{t_2} M \\dot\\theta \\, dt \\\\&amp;= M \\, \\Delta \\theta \\text{ (for constant M)}\\end{aligned}" />
 		<p>
 			The rotation angle \(\theta\) is measured around the same