mirror of https://github.com/ArduPilot/ardupilot
AP_MotorsHeli: Remove unused _dt variable.
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@ -313,7 +313,6 @@ private:
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float _rsc_runup_increment; // the amount we can increase the rotor's estimated speed during each 100hz iteration
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float _rsc_runup_increment; // the amount we can increase the rotor's estimated speed during each 100hz iteration
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float _rotor_speed_estimate; // estimated speed of the main rotor (0~1000)
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float _rotor_speed_estimate; // estimated speed of the main rotor (0~1000)
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int16_t _tail_direct_drive_out; // current ramped speed of output on ch7 when using direct drive variable pitch tail type
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int16_t _tail_direct_drive_out; // current ramped speed of output on ch7 when using direct drive variable pitch tail type
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float _dt; // main loop time
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int16_t _delta_phase_angle; // phase angle dynamic compensation
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int16_t _delta_phase_angle; // phase angle dynamic compensation
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int16_t _roll_radio_passthrough; // roll control PWM direct from radio, used for manual control
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int16_t _roll_radio_passthrough; // roll control PWM direct from radio, used for manual control
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int16_t _pitch_radio_passthrough; // pitch control PWM direct from radio, used for manual control
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int16_t _pitch_radio_passthrough; // pitch control PWM direct from radio, used for manual control
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