use sl.AoA

aenarete · Nov 14, 2024 · 57a2fe9 · 57a2fe9
1 parent 0d3b31b
commit 57a2fe9
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Showing 2 changed files with 7 additions and 7 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_13 = app.kps4.alpha_2
+            # sys_state.var_13 = app.kps4.alpha_2
             sys_state.var_14 = 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
@@ -201,21 +201,21 @@ function plot_aerodynamics(plot_lift_drag = false)
     sl    = log.syslog
 
     if plot_lift_drag
-        display(plotx(sl.time, sl.var_08, sl.var_13, sl.CL2, sl.CD2; 
-                      ylabels=["LoD [-]", L"\alpha_2~[°]", "CL [-]",  "CD [-]"],
+        display(plotx(sl.time, sl.var_08, rad2deg.(sl.AoA), sl.CL2, sl.CD2; 
+                      ylabels=["LoD [-]", L"AoA~[°]", "CL [-]",  "CD [-]"],
                       fig="aerodynamics"))
-        display(plotxy(sl.var_13[2:end], sl.CL2[2:end]; 
+        display(plotxy(rad2deg.(sl.AoA[2:end]), sl.CL2[2:end]; 
                       xlabel="AoA [°]",
                       ylabel="CL [-]",
                       fig="CL as function of AoA"))
-        display(plotxy(sl.var_13[2:end], sl.CD2[2:end]; 
+        display(plotxy(rad2deg.(sl.AoA[2:end]), sl.CD2[2:end]; 
                       xlabel="AoA [°]",
                       ylabel="CD [-]",
                       fig="CD_tot as function of AoA"))
 
     else
-        display(plotx(sl.time, sl.var_08, sl.var_13, sl.var_14, sl.var_15, sl.var_16; 
-                    ylabels=["LoD [-]", L"\alpha_2~[°]", L"\alpha_{3b}~[°]", L"\alpha_{4b}~[°]"],
+        display(plotx(sl.time, sl.var_08, rad2deg.(sl.AoA), sl.var_14, sl.var_15, sl.var_16; 
+                    ylabels=["LoD [-]", L"AoA~[°]", L"\alpha_{3b}~[°]", L"\alpha_{4b}~[°]"],
                     fig="aerodynamics"))
     end
     nothing