Struct mavlink::asluav::SYS_STATUS_DATA

pub struct SYS_STATUS_DATA {

    pub onboard_control_sensors_present: MavSysStatusSensor,
    pub onboard_control_sensors_enabled: MavSysStatusSensor,
    pub onboard_control_sensors_health: MavSysStatusSensor,
    pub load: u16,
    pub voltage_battery: u16,
    pub current_battery: i16,
    pub drop_rate_comm: u16,
    pub errors_comm: u16,
    pub errors_count1: u16,
    pub errors_count2: u16,
    pub errors_count3: u16,
    pub errors_count4: u16,
    pub battery_remaining: i8,
    pub onboard_control_sensors_present_extended: MavSysStatusSensorExtended,
    pub onboard_control_sensors_enabled_extended: MavSysStatusSensorExtended,
    pub onboard_control_sensors_health_extended: MavSysStatusSensorExtended,
}

id: 1 The general system state. If the system is following the MAVLink standard, the system state is mainly defined by three orthogonal states/modes: The system mode, which is either LOCKED (motors shut down and locked), MANUAL (system under RC control), GUIDED (system with autonomous position control, position setpoint controlled manually) or AUTO (system guided by path/waypoint planner). The NAV_MODE defined the current flight state: LIFTOFF (often an open-loop maneuver), LANDING, WAYPOINTS or VECTOR. This represents the internal navigation state machine. The system status shows whether the system is currently active or not and if an emergency occurred. During the CRITICAL and EMERGENCY states the MAV is still considered to be active, but should start emergency procedures autonomously. After a failure occurred it should first move from active to critical to allow manual intervention and then move to emergency after a certain timeout..

Fields

onboard_control_sensors_present: MavSysStatusSensor

Bitmap showing which onboard controllers and sensors are present. Value of 0: not present. Value of 1: present..

onboard_control_sensors_enabled: MavSysStatusSensor

Bitmap showing which onboard controllers and sensors are enabled: Value of 0: not enabled. Value of 1: enabled..

onboard_control_sensors_health: MavSysStatusSensor

Bitmap showing which onboard controllers and sensors have an error (or are operational). Value of 0: error. Value of 1: healthy..

load: u16

Maximum usage in percent of the mainloop time. Values: [0-1000] - should always be below 1000.

voltage_battery: u16

Battery voltage, UINT16_MAX: Voltage not sent by autopilot.

current_battery: i16

Battery current, -1: Current not sent by autopilot.

drop_rate_comm: u16

Communication drop rate, (UART, I2C, SPI, CAN), dropped packets on all links (packets that were corrupted on reception on the MAV).

errors_comm: u16

Communication errors (UART, I2C, SPI, CAN), dropped packets on all links (packets that were corrupted on reception on the MAV).

errors_count1: u16

Autopilot-specific errors.

errors_count2: u16

Autopilot-specific errors.

errors_count3: u16

Autopilot-specific errors.

errors_count4: u16

Autopilot-specific errors.

battery_remaining: i8

Battery energy remaining, -1: Battery remaining energy not sent by autopilot.

onboard_control_sensors_present_extended: MavSysStatusSensorExtended

Bitmap showing which onboard controllers and sensors are present. Value of 0: not present. Value of 1: present..

onboard_control_sensors_enabled_extended: MavSysStatusSensorExtended

Bitmap showing which onboard controllers and sensors are enabled: Value of 0: not enabled. Value of 1: enabled..

onboard_control_sensors_health_extended: MavSysStatusSensorExtended

Bitmap showing which onboard controllers and sensors have an error (or are operational). Value of 0: error. Value of 1: healthy..

Implementations

impl SYS_STATUS_DATA

pub const ENCODED_LEN: usize = 43usize

pub const DEFAULT: Self = _

Trait Implementations

impl Clone for SYS_STATUS_DATA

fn clone(&self) -> SYS_STATUS_DATA

Returns a copy of the value.

fn clone_from(&mut self, source: &Self)

Performs copy-assignment from source.

impl Debug for SYS_STATUS_DATA

fn fmt(&self, f: &mut Formatter<'_>) -> Result

Formats the value using the given formatter.

impl Default for SYS_STATUS_DATA

fn default() -> Self

Returns the “default value” for a type.

impl<'de> Deserialize<'de> for SYS_STATUS_DATA

fn deserialize<__D>(__deserializer: __D) -> Result<Self, __D::Error>where __D: Deserializer<'de>,

Deserialize this value from the given Serde deserializer.

impl MessageData for SYS_STATUS_DATA

type Message = MavMessage

const ID: u32 = 1u32

const NAME: &'static str = "SYS_STATUS"

const EXTRA_CRC: u8 = 124u8

const ENCODED_LEN: usize = 43usize

fn deser(_version: MavlinkVersion, __input: &[u8]) -> Result<Self, ParserError>

fn ser(&self, version: MavlinkVersion, bytes: &mut [u8]) -> usize

impl PartialEq for SYS_STATUS_DATA

fn eq(&self, other: &SYS_STATUS_DATA) -> bool

This method tests for self and other values to be equal, and is used by ==.

fn ne(&self, other: &Rhs) -> bool

This method tests for !=. The default implementation is almost always sufficient, and should not be overridden without very good reason.

impl Serialize for SYS_STATUS_DATA

fn serialize<__S>(&self, __serializer: __S) -> Result<__S::Ok, __S::Error>where __S: Serializer,

Serialize this value into the given Serde serializer.

impl StructuralPartialEq for SYS_STATUS_DATA