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Fix vector indices in inertial speed function of orbital target

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This commit is contained in:
Thorsten Renk 2019-01-18 16:37:35 +02:00
parent 917db66493
commit 2e4193d3a1
1 changed files with 5 additions and 5 deletions
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10
Nasal/orbital_target.nas
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@ -31,7 +31,7 @@ var orbitalTarget = {
t.node_drift = -4361.26 * 1./math.pow(t.radius/1000.0 ,2.0) * math.cos(t.inc_rad);
print ("Drift rate: ", t.node_drift);
#print ("Drift rate: ", t.node_drift);
return t;
},
@ -115,8 +115,8 @@ var orbitalTarget = {
var pos2 = me.compute_inertial_pos(anomaly_rad, me.nl_rad);
var vx = (pos2[0] - pos1[0])/0.1;
var vy = (pos2[0] - pos1[0])/0.1;
var vz = (pos2[0] - pos1[0])/0.1;
var vy = (pos2[1] - pos1[1])/0.1;
var vz = (pos2[2] - pos1[2])/0.1;
return [vx, vy, vz];
},
@ -144,8 +144,8 @@ var orbitalTarget = {
var pos2 = me.compute_inertial_pos(anomaly_rad, nl_rad);
var vx = (pos2[0] - pos1[0])/0.1;
var vy = (pos2[0] - pos1[0])/0.1;
var vz = (pos2[0] - pos1[0])/0.1;
var vy = (pos2[1] - pos1[1])/0.1;
var vz = (pos2[2] - pos1[2])/0.1;
return [vx, vy, vz];
},