Struct mavlink::ardupilotmega::UAVIONIX_ADSB_OUT_DYNAMIC_DATA

pub struct UAVIONIX_ADSB_OUT_DYNAMIC_DATA {

    pub utcTime: u32,
    pub gpsLat: i32,
    pub gpsLon: i32,
    pub gpsAlt: i32,
    pub baroAltMSL: i32,
    pub accuracyHor: u32,
    pub accuracyVert: u16,
    pub accuracyVel: u16,
    pub velVert: i16,
    pub velNS: i16,
    pub VelEW: i16,
    pub state: UavionixAdsbOutDynamicState,
    pub squawk: u16,
    pub gpsFix: UavionixAdsbOutDynamicGpsFix,
    pub numSats: u8,
    pub emergencyStatus: UavionixAdsbEmergencyStatus,
}

id: 10002 Dynamic data used to generate ADS-B out transponder data (send at 5Hz).

Fields

utcTime: u32

UTC time in seconds since GPS epoch (Jan 6, 1980). If unknown set to UINT32_MAX.

gpsLat: i32

Latitude WGS84 (deg * 1E7). If unknown set to INT32_MAX.

gpsLon: i32

Longitude WGS84 (deg * 1E7). If unknown set to INT32_MAX.

gpsAlt: i32

Altitude (WGS84). UP +ve. If unknown set to INT32_MAX.

baroAltMSL: i32

Barometric pressure altitude (MSL) relative to a standard atmosphere of 1013.2 mBar and NOT bar corrected altitude (m * 1E-3). (up +ve). If unknown set to INT32_MAX.

accuracyHor: u32

Horizontal accuracy in mm (m * 1E-3). If unknown set to UINT32_MAX.

accuracyVert: u16

Vertical accuracy in cm. If unknown set to UINT16_MAX.

accuracyVel: u16

Velocity accuracy in mm/s (m * 1E-3). If unknown set to UINT16_MAX.

velVert: i16

GPS vertical speed in cm/s. If unknown set to INT16_MAX.

velNS: i16

North-South velocity over ground in cm/s North +ve. If unknown set to INT16_MAX.

VelEW: i16

East-West velocity over ground in cm/s East +ve. If unknown set to INT16_MAX.

state: UavionixAdsbOutDynamicState

ADS-B transponder dynamic input state flags.

squawk: u16

Mode A code (typically 1200 [0x04B0] for VFR).

gpsFix: UavionixAdsbOutDynamicGpsFix

0-1: no fix, 2: 2D fix, 3: 3D fix, 4: DGPS, 5: RTK.

numSats: u8

Number of satellites visible. If unknown set to UINT8_MAX.

emergencyStatus: UavionixAdsbEmergencyStatus

Emergency status.

Implementations

impl UAVIONIX_ADSB_OUT_DYNAMIC_DATA

pub const ENCODED_LEN: usize = 41usize

pub const DEFAULT: Self = _

Trait Implementations

impl Clone for UAVIONIX_ADSB_OUT_DYNAMIC_DATA

fn clone(&self) -> UAVIONIX_ADSB_OUT_DYNAMIC_DATA

Returns a copy of the value.

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

Performs copy-assignment from source.

impl Debug for UAVIONIX_ADSB_OUT_DYNAMIC_DATA

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

Formats the value using the given formatter.

impl Default for UAVIONIX_ADSB_OUT_DYNAMIC_DATA

fn default() -> Self

Returns the “default value” for a type.

impl<'de> Deserialize<'de> for UAVIONIX_ADSB_OUT_DYNAMIC_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 UAVIONIX_ADSB_OUT_DYNAMIC_DATA

type Message = MavMessage

const ID: u32 = 10_002u32

const NAME: &'static str = "UAVIONIX_ADSB_OUT_DYNAMIC"

const EXTRA_CRC: u8 = 186u8

const ENCODED_LEN: usize = 41usize

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

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

impl PartialEq for UAVIONIX_ADSB_OUT_DYNAMIC_DATA

fn eq(&self, other: &UAVIONIX_ADSB_OUT_DYNAMIC_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 UAVIONIX_ADSB_OUT_DYNAMIC_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 UAVIONIX_ADSB_OUT_DYNAMIC_DATA