Da Vinci Firmware 1
Firmware for the DaVinci-M rocket avionics board.
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Data Fields
linear_acceleration_t Struct Reference
Core Flight Logic » Flight State Machine (FSM)

Represents a 3-axis linear acceleration vector from an IMU. More...

#include <flight_control.h>

Data Fields

float_t accX
 Acceleration along the X-axis in m/s^2.
 
float_t accY
 Acceleration along the Y-axis in m/s^2.
 
float_t accZ
 Acceleration along the Z-axis in m/s^2.
 

Detailed Description

Represents a 3-axis linear acceleration vector from an IMU.

Definition at line 48 of file flight_control.h.

Field Documentation

◆ accX

float_t linear_acceleration_t::accX

Acceleration along the X-axis in m/s^2.

Definition at line 49 of file flight_control.h.

Referenced by check_Calibrating_phase(), and StartFSM().

◆ accY

float_t linear_acceleration_t::accY

Acceleration along the Y-axis in m/s^2.

Definition at line 50 of file flight_control.h.

Referenced by StartFSM().

◆ accZ

float_t linear_acceleration_t::accZ

Acceleration along the Z-axis in m/s^2.

Definition at line 51 of file flight_control.h.

Referenced by StartFSM().

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