Orbital Maneuvers - Orbital and Celestial Mechanics Website
Orbital Maneuvers - Orbital and Celestial Mechanics Website
Orbital Maneuvers - Orbital and Celestial Mechanics Website
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
chaser initial conditions<br />
-------------------------<br />
altitude 500.000000 kilometers<br />
<strong>Orbital</strong> <strong>Mechanics</strong> with MATLAB<br />
sma (km) eccentricity inclination (deg) argper (deg)<br />
+6.87813630000000e+003 +0.00000000000000e+000 +0.00000000000000e+000 +0.00000000000000e+000<br />
raan (deg) true anomaly (deg) arglat (deg) period (min)<br />
+0.00000000000000e+000 +4.50000000000000e+001 +4.50000000000000e+001 +9.46162866922553e+001<br />
rx (km) ry (km) rz (km) rmag (km)<br />
+4.86357681965535e+003 +4.86357681965535e+003 +0.00000000000000e+000 +6.87813630000000e+003<br />
vx (kps) vy (kps) vz (kps) vmag (kps)<br />
-5.38292709812771e+000 +5.38292709812772e+000 +0.00000000000000e+000 +7.61260850743786e+000<br />
target initial conditions<br />
-------------------------<br />
altitude 5000.000000 kilometers<br />
sma (km) eccentricity inclination (deg) argper (deg)<br />
+1.13781363000000e+004 +0.00000000000000e+000 +0.00000000000000e+000 +0.00000000000000e+000<br />
raan (deg) true anomaly (deg) arglat (deg) period (min)<br />
+0.00000000000000e+000 +9.00000000000000e+001 +9.00000000000000e+001 +2.01310501632031e+002<br />
rx (km) ry (km) rz (km) rmag (km)<br />
+6.96709910002865e-013 +1.13781363000000e+004 +0.00000000000000e+000 +1.13781363000000e+004<br />
vx (kps) vy (kps) vz (kps) vmag (kps)<br />
-5.91879528089421e+000 +3.62421684777778e-016 +0.00000000000000e+000 +5.91879528089421e+000<br />
transfer orbit initial conditions<br />
---------------------------------<br />
sma (km) eccentricity inclination (deg) argper (deg)<br />
+9.12813630000000e+003 +2.46490622625782e-001 +0.00000000000000e+000 +3.53571678494045e+002<br />
raan (deg) true anomaly (deg) arglat (deg) period (min)<br />
+0.00000000000000e+000 +0.00000000000000e+000 +3.53571678494045e+002 +1.44654819447959e+002<br />
rx (km) ry (km) rz (km) rmag (km)<br />
+6.83489138174017e+003 -7.70077113795533e+002 +0.00000000000000e+000 +6.87813630000000e+003<br />
vx (kps) vy (kps) vz (kps) vmag (kps)<br />
+9.51571536023532e-001 +8.44576208559208e+000 +0.00000000000000e+000 +8.49919911489282e+000<br />
trajectory times<br />
----------------<br />
transfer time-of-flight 4339.644583 seconds<br />
72.327410 minutes<br />
wait time 10542.961601 seconds<br />
175.716027 minutes<br />
total mission time 14882.606185 seconds<br />
248.043436 minutes<br />
page 38
Change language