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Revert initial setting
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@200km
200km committed Dec 17, 2024
1 parent f365e39 commit 5472af4
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4 changes: 2 additions & 2 deletions settings/sample_satellite/satellite.ini
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// RK4 : Attitude Propagation with RK4 including disturbances and control torque
// CANTILEVER_VIBRATION : Attitude Propagation with the consideration of the cantilever vibration (flexible structure) including disturbances and control torque.
// CONTROLLED : Attitude Calculation with Controlled Attitude mode. All disturbances and control torque are ignored.
propagate_mode = CONTROLLED
propagate_mode = RK4

// Initialize Attitude mode
// MANUAL : Initialize Quaternion_i2b manually below
Expand Down Expand Up @@ -37,7 +37,7 @@ initial_torque_b_Nm(2) = 0.000
// GROUND_SPEED_DIRECTION_POINTING
// ORBIT_NORMAL_POINTING
// EARTH_SURFACE_POINTING
main_mode = EARTH_SURFACE_POINTING
main_mode = INERTIAL_STABILIZE
sub_mode = SUN_POINTING

// Pointing direction @ body frame for main pointing mode
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