PX4 Firmware
PX4 Autopilot Software http://px4.io
tecs_status.h
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33 
34 /* Auto-generated by genmsg_cpp from file tecs_status.msg */
35 
36 
37 #pragma once
38 
39 
40 #include <uORB/uORB.h>
41 
42 
43 #ifndef __cplusplus
44 #define TECS_STATUS_TECS_MODE_NORMAL 0
45 #define TECS_STATUS_TECS_MODE_UNDERSPEED 1
46 #define TECS_STATUS_TECS_MODE_TAKEOFF 2
47 #define TECS_STATUS_TECS_MODE_LAND 3
48 #define TECS_STATUS_TECS_MODE_LAND_THROTTLELIM 4
49 #define TECS_STATUS_TECS_MODE_BAD_DESCENT 5
50 #define TECS_STATUS_TECS_MODE_CLIMBOUT 6
51 
52 #endif
53 
54 
55 #ifdef __cplusplus
56 struct __EXPORT tecs_status_s {
57 #else
58 struct tecs_status_s {
59 #endif
60  uint64_t timestamp;
61  float altitude_sp;
64  float height_rate;
65  float airspeed_sp;
74  float pitch_integ;
75  uint8_t mode;
76  uint8_t _padding0[7]; // required for logger
77 
78 
79 #ifdef __cplusplus
80  static constexpr uint8_t TECS_MODE_NORMAL = 0;
81  static constexpr uint8_t TECS_MODE_UNDERSPEED = 1;
82  static constexpr uint8_t TECS_MODE_TAKEOFF = 2;
83  static constexpr uint8_t TECS_MODE_LAND = 3;
84  static constexpr uint8_t TECS_MODE_LAND_THROTTLELIM = 4;
85  static constexpr uint8_t TECS_MODE_BAD_DESCENT = 5;
86  static constexpr uint8_t TECS_MODE_CLIMBOUT = 6;
87 
88 #endif
89 };
90 
91 /* register this as object request broker structure */
92 ORB_DECLARE(tecs_status);
93 
94 
95 #ifdef __cplusplus
96 void print_message(const tecs_status_s& message);
97 #endif
float total_energy_rate_error
Definition: tecs_status.h:71
float height_rate
Definition: tecs_status.h:64
API for the uORB lightweight object broker.
float airspeed_filtered
Definition: tecs_status.h:66
Definition: I2C.hpp:51
uint8_t mode
Definition: tecs_status.h:75
float throttle_integ
Definition: tecs_status.h:73
float altitude_sp
Definition: tecs_status.h:61
float pitch_integ
Definition: tecs_status.h:74
float altitude_filtered
Definition: tecs_status.h:62
float energy_distribution_error
Definition: tecs_status.h:70
ORB_DECLARE(tecs_status)
float airspeed_sp
Definition: tecs_status.h:65
uint64_t timestamp
Definition: tecs_status.h:60
float energy_distribution_rate_error
Definition: tecs_status.h:72
float airspeed_derivative
Definition: tecs_status.h:68
float height_rate_setpoint
Definition: tecs_status.h:63
float airspeed_derivative_sp
Definition: tecs_status.h:67
float total_energy_error
Definition: tecs_status.h:69