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Revert initial setting
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settings/sample_satellite/satellite.ini

Lines changed: 2 additions & 2 deletions
Original file line numberDiff line numberDiff line change
@@ -3,7 +3,7 @@
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// RK4 : Attitude Propagation with RK4 including disturbances and control torque
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// CANTILEVER_VIBRATION : Attitude Propagation with the consideration of the cantilever vibration (flexible structure) including disturbances and control torque.
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// CONTROLLED : Attitude Calculation with Controlled Attitude mode. All disturbances and control torque are ignored.
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propagate_mode = CONTROLLED
6+
propagate_mode = RK4
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// Initialize Attitude mode
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// MANUAL : Initialize Quaternion_i2b manually below
@@ -37,7 +37,7 @@ initial_torque_b_Nm(2) = 0.000
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// GROUND_SPEED_DIRECTION_POINTING
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// ORBIT_NORMAL_POINTING
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// EARTH_SURFACE_POINTING
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main_mode = EARTH_SURFACE_POINTING
40+
main_mode = INERTIAL_STABILIZE
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sub_mode = SUN_POINTING
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// Pointing direction @ body frame for main pointing mode

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