diff options
Diffstat (limited to 'apps/sdlog/sdlog_ringbuffer.h')
| -rw-r--r-- | apps/sdlog/sdlog_ringbuffer.h | 5 |
1 files changed, 5 insertions, 0 deletions
diff --git a/apps/sdlog/sdlog_ringbuffer.h b/apps/sdlog/sdlog_ringbuffer.h index 68fff3a91..f7fc0d450 100644 --- a/apps/sdlog/sdlog_ringbuffer.h +++ b/apps/sdlog/sdlog_ringbuffer.h @@ -54,6 +54,8 @@ struct sdlog_sysvector { float control[4]; /**< roll, pitch, yaw [-1..1], thrust [0..1] */ float actuators[8]; /**< motor 1-8, in motor units (PWM: 1000-2000,AR.Drone: 0-512) */ float vbat; /**< battery voltage in [volt] */ + float bat_current; /**< battery discharge current */ + float bat_discharged; /**< discharged energy in mAh */ float adc[3]; /**< remaining auxiliary ADC ports [volt] */ float local_position[3]; /**< tangent plane mapping into x,y,z [m] */ int32_t gps_raw_position[3]; /**< latitude [degrees] north, longitude [degrees] east, altitude above MSL [millimeter] */ @@ -62,6 +64,9 @@ struct sdlog_sysvector { float vicon[6]; /**< Vicon ground truth x, y, z and roll, pitch, yaw */ float control_effective[4]; /**< roll, pitch, yaw [-1..1], thrust [0..1] */ float flow[6]; /**< flow raw x, y, flow metric x, y, flow ground dist, flow quality */ + float diff_pressure; /**< differential pressure */ + float ind_airspeed; /**< indicated airspeed */ + float true_airspeed; /**< true airspeed */ }; #pragma pack(pop) |