Da Vinci Firmware 1
Firmware for the DaVinci-M rocket avionics board.
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estimation_output_t Struct Reference

Holds the primary outputs of the state estimation filter (e.g., Kalman filter). More...

#include <flight_control.h>

Data Fields

float_t height
 Vertical altitude above ground level in meters (m).
 
float_t velocity
 Vertical velocity in meters per second (m/s).
 
float_t acceleration
 Vertical acceleration in meters per second squared (m/s^2).
 

Detailed Description

Holds the primary outputs of the state estimation filter (e.g., Kalman filter).

Definition at line 58 of file flight_control.h.

Field Documentation

◆ acceleration

float_t estimation_output_t::acceleration

Vertical acceleration in meters per second squared (m/s^2).

Definition at line 61 of file flight_control.h.

Referenced by StartFSM().

◆ height

float_t estimation_output_t::height

Vertical altitude above ground level in meters (m).

Definition at line 59 of file flight_control.h.

Referenced by check_AbcsDeployed_phase(), check_Burning_phase(), check_Calibrating_phase(), check_Drogue_phase(), check_Liftoff_phase(), and StartFSM().

◆ velocity

float_t estimation_output_t::velocity

Vertical velocity in meters per second (m/s).

Definition at line 60 of file flight_control.h.

Referenced by check_Main_phase(), and StartFSM().


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