Struct mavlink::cubepilot::SIM_STATE_DATA

pub struct SIM_STATE_DATA {

    pub q1: f32,
    pub q2: f32,
    pub q3: f32,
    pub q4: f32,
    pub roll: f32,
    pub pitch: f32,
    pub yaw: f32,
    pub xacc: f32,
    pub yacc: f32,
    pub zacc: f32,
    pub xgyro: f32,
    pub ygyro: f32,
    pub zgyro: f32,
    pub lat: f32,
    pub lon: f32,
    pub alt: f32,
    pub std_dev_horz: f32,
    pub std_dev_vert: f32,
    pub vn: f32,
    pub ve: f32,
    pub vd: f32,
    pub lat_int: i32,
    pub lon_int: i32,
}

id: 108 Status of simulation environment, if used.

Fields

q1: f32

True attitude quaternion component 1, w (1 in null-rotation).

q2: f32

True attitude quaternion component 2, x (0 in null-rotation).

q3: f32

True attitude quaternion component 3, y (0 in null-rotation).

q4: f32

True attitude quaternion component 4, z (0 in null-rotation).

roll: f32

Attitude roll expressed as Euler angles, not recommended except for human-readable outputs.

pitch: f32

Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs.

yaw: f32

Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs.

xacc: f32

X acceleration.

yacc: f32

Y acceleration.

zacc: f32

Z acceleration.

xgyro: f32

Angular speed around X axis.

ygyro: f32

Angular speed around Y axis.

zgyro: f32

Angular speed around Z axis.

lat: f32

Latitude (lower precision). Both this and the lat_int field should be set..

lon: f32

Longitude (lower precision). Both this and the lon_int field should be set..

alt: f32

Altitude.

std_dev_horz: f32

Horizontal position standard deviation.

std_dev_vert: f32

Vertical position standard deviation.

vn: f32

True velocity in north direction in earth-fixed NED frame.

ve: f32

True velocity in east direction in earth-fixed NED frame.

vd: f32

True velocity in down direction in earth-fixed NED frame.

lat_int: i32

Latitude (higher precision). If 0, recipients should use the lat field value (otherwise this field is preferred)..

lon_int: i32

Longitude (higher precision). If 0, recipients should use the lon field value (otherwise this field is preferred)..

Implementations

impl SIM_STATE_DATA

pub const ENCODED_LEN: usize = 92usize

pub const DEFAULT: Self = _

Trait Implementations

impl Clone for SIM_STATE_DATA

fn clone(&self) -> SIM_STATE_DATA

Returns a copy of the value.

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

Performs copy-assignment from source.

impl Debug for SIM_STATE_DATA

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

Formats the value using the given formatter.

impl Default for SIM_STATE_DATA

fn default() -> Self

Returns the “default value” for a type.

impl<'de> Deserialize<'de> for SIM_STATE_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 SIM_STATE_DATA

type Message = MavMessage

const ID: u32 = 108u32

const NAME: &'static str = "SIM_STATE"

const EXTRA_CRC: u8 = 32u8

const ENCODED_LEN: usize = 92usize

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

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

impl PartialEq for SIM_STATE_DATA

fn eq(&self, other: &SIM_STATE_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 SIM_STATE_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 SIM_STATE_DATA