tecs_status_s Struct Reference

#include <tecs_status.h>

Collaboration diagram for tecs_status_s:

Public Attributes
uint64_t	timestamp
float	altitude_sp
float	altitude_filtered
float	height_rate_setpoint
float	height_rate
float	airspeed_sp
float	airspeed_filtered
float	airspeed_derivative_sp
float	airspeed_derivative
float	total_energy_error
float	energy_distribution_error
float	total_energy_rate_error
float	energy_distribution_rate_error
float	throttle_integ
float	pitch_integ
uint8_t	mode
uint8_t	_padding0 [7]

Detailed Description

Definition at line 58 of file tecs_status.h.

Member Data Documentation

_padding0

uint8_t tecs_status_s::_padding0[7]

Definition at line 76 of file tecs_status.h.

airspeed_derivative

float tecs_status_s::airspeed_derivative

Definition at line 68 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

airspeed_derivative_sp

float tecs_status_s::airspeed_derivative_sp

Definition at line 67 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

airspeed_filtered

float tecs_status_s::airspeed_filtered

Definition at line 66 of file tecs_status.h.

Referenced by MavlinkStreamNavControllerOutput::send(), and FixedwingPositionControl::tecs_status_publish().

airspeed_sp

float tecs_status_s::airspeed_sp

Definition at line 65 of file tecs_status.h.

Referenced by MavlinkStreamNavControllerOutput::send(), FixedwingPositionControl::tecs_status_publish(), and MavlinkStreamHighLatency2::update_tecs_status().

altitude_filtered

float tecs_status_s::altitude_filtered

Definition at line 62 of file tecs_status.h.

Referenced by VtolType::check_quadchute_condition(), MavlinkStreamNavControllerOutput::send(), and FixedwingPositionControl::tecs_status_publish().

altitude_sp

float tecs_status_s::altitude_sp

Definition at line 61 of file tecs_status.h.

Referenced by VtolType::check_quadchute_condition(), MavlinkStreamNavControllerOutput::send(), FixedwingPositionControl::tecs_status_publish(), and MavlinkStreamHighLatency2::write_tecs_status().

energy_distribution_error

float tecs_status_s::energy_distribution_error

Definition at line 70 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

energy_distribution_rate_error

float tecs_status_s::energy_distribution_rate_error

Definition at line 72 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

height_rate

float tecs_status_s::height_rate

Definition at line 64 of file tecs_status.h.

Referenced by VtolType::check_quadchute_condition(), and FixedwingPositionControl::tecs_status_publish().

height_rate_setpoint

float tecs_status_s::height_rate_setpoint

Definition at line 63 of file tecs_status.h.

Referenced by VtolType::check_quadchute_condition(), and FixedwingPositionControl::tecs_status_publish().

mode

uint8_t tecs_status_s::mode

Definition at line 75 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

pitch_integ

float tecs_status_s::pitch_integ

Definition at line 74 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

throttle_integ

float tecs_status_s::throttle_integ

Definition at line 73 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

timestamp

uint64_t tecs_status_s::timestamp

Definition at line 60 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish(), and VtolType::update_fw_state().

total_energy_error

float tecs_status_s::total_energy_error

Definition at line 69 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

total_energy_rate_error

float tecs_status_s::total_energy_rate_error

Definition at line 71 of file tecs_status.h.

Referenced by FixedwingPositionControl::tecs_status_publish().

---

The documentation for this struct was generated from the following file:

• build/doxygen/uORB/topics/tecs_status.h