Adjust demo scenario to use impulsive maneuver

arda-guler · arda-guler · commit cfa8348950b3 · 2023-01-19T12:25:34.000+03:00
diff --git a/scenarios/GMAT.obf b/scenarios/GMAT.obf
@@ -2,11 +2,8 @@
 ;
 lock_origin Earth
 clear traj_visuals
-delta_t 0.25
 create_plot pl_alt alt orbiter Earth 0 18000
 create_plot pl_vel vel_mag orbiter Earth 0 18000
-auto_dt 5998 0.00390625
-auto_dt 6002 0.25
 rapid_compute 5900
 output_rate 100
 ;
diff --git a/scenarios/GMAT.osf b/scenarios/GMAT.osf
@@ -11,5 +11,5 @@ B|Luna|data/models/miniluna.obj|73420000000000000000000|1737000|[0.8,0.8,0.8]|[3
 V|orbiter|data/models/miniprobe.obj|[0.0,0.8,0.7]|[7100E3,0,1300E3]|[-1000,0,7350]
 
 ;Maneuvers
-M|mnv_impulsive|const_accel|orbiter|Earth|prograde|1000|6000|1
+M|mnv_test|impulsive|orbiter|Earth|prograde|1000|6000
 

Original file line number	Diff line number	Diff line change
`@@ -2,11 +2,8 @@`
`2`	`2`	`;`
`3`	`3`	`lock_origin Earth`
`4`	`4`	`clear traj_visuals`
`5`		`-delta_t 0.25`
`6`	`5`	`create_plot pl_alt alt orbiter Earth 0 18000`
`7`	`6`	`create_plot pl_vel vel_mag orbiter Earth 0 18000`
`8`		`-auto_dt 5998 0.00390625`
`9`		`-auto_dt 6002 0.25`
`10`	`7`	`rapid_compute 5900`
`11`	`8`	`output_rate 100`
`12`	`9`	`;`