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new manual_control_switches msg (split out of manual_control_setpoint) (#16270)
- split out switches from manual_control_setpoint into new message manual_control_switches
- manual_control_switches published at minimal rate (~ 1 Hz) or immediately on change
- simple switch debounce in rc_update (2 consecutive identical decodes required)
- manual_control_switches logged at full rate rather than sampled at (5-10% of messages logged)
- manual_control_setpoint publish at minimal rate unless changing
- commander handle landing gear switch for manual modes
- processing of mode_slot and mode_switch is now split so we only do one or the other (not both)
- a future step will be to finally drop mode_switch and accompanying switches entirely
Co-authored-by: Matthias Grob <maetugr@gmail.com>
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@@ -85,12 +85,6 @@ private:
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*/
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void parameters_updated();
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/**
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* Get the landing gear state based on the manual control switch position
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* @return vehicle_attitude_setpoint_s::LANDING_GEAR_UP or vehicle_attitude_setpoint_s::LANDING_GEAR_DOWN
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*/
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float get_landing_gear_state();
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RateControl _rate_control; ///< class for rate control calculations
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uORB::Subscription _battery_status_sub{ORB_ID(battery_status)};
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@@ -111,7 +105,6 @@ private:
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uORB::Publication<landing_gear_s> _landing_gear_pub{ORB_ID(landing_gear)};
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uORB::Publication<vehicle_rates_setpoint_s> _v_rates_sp_pub{ORB_ID(vehicle_rates_setpoint)}; /**< rate setpoint publication */
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landing_gear_s _landing_gear{};
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manual_control_setpoint_s _manual_control_setpoint{};
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vehicle_control_mode_s _v_control_mode{};
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vehicle_status_s _vehicle_status{};
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@@ -128,10 +121,10 @@ private:
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float _thrust_sp{0.0f}; /**< thrust setpoint */
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bool _gear_state_initialized{false}; /**< true if the gear state has been initialized */
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hrt_abstime _last_run{0};
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int8_t _landing_gear{landing_gear_s::GEAR_DOWN};
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DEFINE_PARAMETERS(
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(ParamFloat<px4::params::MC_ROLLRATE_P>) _param_mc_rollrate_p,
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(ParamFloat<px4::params::MC_ROLLRATE_I>) _param_mc_rollrate_i,
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