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NinjaFlight
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NinjaFlight
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#include <mavlink_msg_sim_state.h>
Data Fields | |
| float | q1 |
| True attitude quaternion component 1, w (1 in null-rotation) More... | |
| float | q2 |
| True attitude quaternion component 2, x (0 in null-rotation) More... | |
| float | q3 |
| True attitude quaternion component 3, y (0 in null-rotation) More... | |
| float | q4 |
| True attitude quaternion component 4, z (0 in null-rotation) More... | |
| float | roll |
| Attitude roll expressed as Euler angles, not recommended except for human-readable outputs. More... | |
| float | pitch |
| Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs. More... | |
| float | yaw |
| Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs. More... | |
| float | xacc |
| X acceleration m/s/s. More... | |
| float | yacc |
| Y acceleration m/s/s. More... | |
| float | zacc |
| Z acceleration m/s/s. More... | |
| float | xgyro |
| Angular speed around X axis rad/s. More... | |
| float | ygyro |
| Angular speed around Y axis rad/s. More... | |
| float | zgyro |
| Angular speed around Z axis rad/s. More... | |
| float | lat |
| Latitude in degrees. More... | |
| float | lon |
| Longitude in degrees. More... | |
| float | alt |
| Altitude in meters. More... | |
| float | std_dev_horz |
| Horizontal position standard deviation. More... | |
| float | std_dev_vert |
| Vertical position standard deviation. More... | |
| float | vn |
| True velocity in m/s in NORTH direction in earth-fixed NED frame. More... | |
| float | ve |
| True velocity in m/s in EAST direction in earth-fixed NED frame. More... | |
| float | vd |
| True velocity in m/s in DOWN direction in earth-fixed NED frame. More... | |
| float __mavlink_sim_state_t::alt |
Altitude in meters.
| float __mavlink_sim_state_t::lat |
Latitude in degrees.
| float __mavlink_sim_state_t::lon |
Longitude in degrees.
| float __mavlink_sim_state_t::pitch |
Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs.
| float __mavlink_sim_state_t::q1 |
True attitude quaternion component 1, w (1 in null-rotation)
| float __mavlink_sim_state_t::q2 |
True attitude quaternion component 2, x (0 in null-rotation)
| float __mavlink_sim_state_t::q3 |
True attitude quaternion component 3, y (0 in null-rotation)
| float __mavlink_sim_state_t::q4 |
True attitude quaternion component 4, z (0 in null-rotation)
| float __mavlink_sim_state_t::roll |
Attitude roll expressed as Euler angles, not recommended except for human-readable outputs.
| float __mavlink_sim_state_t::std_dev_horz |
Horizontal position standard deviation.
| float __mavlink_sim_state_t::std_dev_vert |
Vertical position standard deviation.
| float __mavlink_sim_state_t::vd |
True velocity in m/s in DOWN direction in earth-fixed NED frame.
| float __mavlink_sim_state_t::ve |
True velocity in m/s in EAST direction in earth-fixed NED frame.
| float __mavlink_sim_state_t::vn |
True velocity in m/s in NORTH direction in earth-fixed NED frame.
| float __mavlink_sim_state_t::xacc |
X acceleration m/s/s.
| float __mavlink_sim_state_t::xgyro |
Angular speed around X axis rad/s.
| float __mavlink_sim_state_t::yacc |
Y acceleration m/s/s.
| float __mavlink_sim_state_t::yaw |
Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs.
| float __mavlink_sim_state_t::ygyro |
Angular speed around Y axis rad/s.
| float __mavlink_sim_state_t::zacc |
Z acceleration m/s/s.
| float __mavlink_sim_state_t::zgyro |
Angular speed around Z axis rad/s.
1.8.7 
