Struct mavlink::uavionix::ORBIT_EXECUTION_STATUS_DATA

pub struct ORBIT_EXECUTION_STATUS_DATA {
    pub time_usec: u64,
    pub radius: f32,
    pub x: i32,
    pub y: i32,
    pub z: f32,
    pub frame: MavFrame,
}

Available on crate feature uavionix only.

id: 360 Vehicle status report that is sent out while orbit execution is in progress (see MAV_CMD_DO_ORBIT)..

Fields

time_usec: u64

Timestamp (UNIX Epoch time or time since system boot). The receiving end can infer timestamp format (since 1.1.1970 or since system boot) by checking for the magnitude of the number..

radius: f32

Radius of the orbit circle. Positive values orbit clockwise, negative values orbit counter-clockwise..

x: i32

X coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7..

y: i32

Y coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7..

z: f32

Altitude of center point. Coordinate system depends on frame field..

frame: MavFrame

The coordinate system of the fields: x, y, z..

Implementations

impl ORBIT_EXECUTION_STATUS_DATA

pub const ENCODED_LEN: usize = 25usize

pub const DEFAULT: Self = _

Trait Implementations

impl Clone for ORBIT_EXECUTION_STATUS_DATA

fn clone(&self) -> ORBIT_EXECUTION_STATUS_DATA

Returns a copy of the value.

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

Performs copy-assignment from source.

impl Debug for ORBIT_EXECUTION_STATUS_DATA

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

Formats the value using the given formatter.

impl Default for ORBIT_EXECUTION_STATUS_DATA

fn default() -> Self

Returns the “default value” for a type.

impl<'de> Deserialize<'de> for ORBIT_EXECUTION_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 ORBIT_EXECUTION_STATUS_DATA

const ID: u32 = 360u32

const NAME: &'static str = "ORBIT_EXECUTION_STATUS"

const EXTRA_CRC: u8 = 11u8

const ENCODED_LEN: usize = 25usize

type Message = MavMessage

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

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

impl PartialEq for ORBIT_EXECUTION_STATUS_DATA

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

Tests for self and other values to be equal, and is used by ==.

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

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

impl Serialize for ORBIT_EXECUTION_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 ORBIT_EXECUTION_STATUS_DATA