use acc

aenarete · Nov 15, 2024 · 1db7846 · 1db7846
1 parent 0bebe97
commit 1db7846
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Showing 2 changed files with 3 additions and 3 deletions.
diff --git a/examples/autopilot.jl b/examples/autopilot.jl
@@ -213,7 +213,7 @@ function simulate(integrator, stopped=true)
 
             sys_state.var_11 = app.ssc.fpp.fpca.fpc.est_chi_dot
             sys_state.var_12 = app.ssc.fpp.fpca.fpc.c2
-            sys_state.var_14 = norm(acc)
+            sys_state.acc = norm(acc)
             sys_state.var_15 = app.kps4.alpha_3b 
             sys_state.var_16 = app.kps4.alpha_4b 
 

diff --git a/examples/plots.jl b/examples/plots.jl
@@ -50,7 +50,7 @@ function plot_power()
         en +=  sl.force[i]*sl.v_reelout[i]*app.dt
         energy[i] = en
     end
-    display(plotx(log.syslog.time, sl.force, sl.v_reelout, sl.force.*sl.v_reelout, energy./3600, sl.var_14;
+    display(plotx(log.syslog.time, sl.force, sl.v_reelout, sl.force.*sl.v_reelout, energy./3600, sl.acc;
             ylabels=["force [N]", L"v_\mathrm{ro}~[m/s]", L"P_\mathrm{m}~[W]", "Energy [Wh]", "acc [m/s^2]"],
             fig="power"))
     nothing
@@ -214,7 +214,7 @@ function plot_aerodynamics(plot_lift_drag = false)
                       fig="CD_tot as function of AoA"))
 
     else
-        display(plotx(sl.time, sl.var_08, rad2deg.(sl.AoA), sl.var_14, sl.var_15, sl.var_16; 
+        display(plotx(sl.time, sl.var_08, rad2deg.(sl.AoA), sl.acc, sl.var_15, sl.var_16; 
                     ylabels=["LoD [-]", L"AoA~[°]", L"\alpha_{3b}~[°]", L"\alpha_{4b}~[°]"],
                     fig="aerodynamics"))
     end