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fw_att_control: update orb_publish to uORB::Publication<>

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This commit is contained in:
Daniel Agar
2019-09-02 16:20:44 -04:00
parent b0f82ee8ac
commit e83026f106
2 changed files with 14 additions and 33 deletions
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src/modules/fw_att_control/FixedwingAttitudeControl.hpp
+10 -7
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@@ -47,6 +47,8 @@
#include <parameters/param.h>
#include <perf/perf_counter.h>
#include <px4_platform_common/px4_work_queue/WorkItem.hpp>
#include <uORB/Publication.hpp>
#include <uORB/PublicationMulti.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/SubscriptionCallback.hpp>
#include <uORB/topics/actuator_controls.h>
@@ -108,14 +110,15 @@ private:
uORB::SubscriptionData<airspeed_s> _airspeed_sub{ORB_ID(airspeed)};
orb_advert_t _rate_sp_pub{nullptr}; /**< rate setpoint publication */
orb_advert_t _attitude_sp_pub{nullptr}; /**< attitude setpoint point */
orb_advert_t _actuators_0_pub{nullptr}; /**< actuator control group 0 setpoint */
orb_advert_t _actuators_2_pub{nullptr}; /**< actuator control group 1 setpoint (Airframe) */
orb_advert_t _rate_ctrl_status_pub{nullptr}; /**< rate controller status publication */
uORB::Publication<actuator_controls_s> _actuators_2_pub{ORB_ID(actuator_controls_2)}; /**< actuator control group 1 setpoint (Airframe) */
uORB::Publication<vehicle_rates_setpoint_s> _rate_sp_pub{ORB_ID(vehicle_rates_setpoint)}; /**< rate setpoint publication */
uORB::PublicationMulti<rate_ctrl_status_s> _rate_ctrl_status_pub{ORB_ID(rate_ctrl_status)}; /**< rate controller status publication */
orb_id_t _actuators_id{nullptr}; // pointer to correct actuator controls0 uORB metadata structure
orb_id_t _attitude_setpoint_id{nullptr};
orb_id_t _attitude_setpoint_id{nullptr};
orb_advert_t _attitude_sp_pub{nullptr}; /**< attitude setpoint point */
orb_id_t _actuators_id{nullptr}; /**< pointer to correct actuator controls0 uORB metadata structure */
orb_advert_t _actuators_0_pub{nullptr}; /**< actuator control group 0 setpoint */
actuator_controls_s _actuators {}; /**< actuator control inputs */
actuator_controls_s _actuators_airframe {}; /**< actuator control inputs */