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Remove unused q_e flag
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@@ -21,8 +21,6 @@ bool R_valid # Set to true if rotation matrix is valid
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# For quaternion-based attitude control
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float32[4] q_d # Desired quaternion for quaternion control
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bool q_d_valid # Set to true if quaternion vector is valid
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float32[4] q_e # Attitude error in quaternion
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bool q_e_valid # Set to true if quaternion error vector is valid
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float32 thrust # Thrust in Newton the power system should generate
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