Struct HIL_STATE_DATA 

pub struct HIL_STATE_DATA {

    pub time_usec: u64,
    pub roll: f32,
    pub pitch: f32,
    pub yaw: f32,
    pub rollspeed: f32,
    pub pitchspeed: f32,
    pub yawspeed: f32,
    pub lat: i32,
    pub lon: i32,
    pub alt: i32,
    pub vx: i16,
    pub vy: i16,
    pub vz: i16,
    pub xacc: i16,
    pub yacc: i16,
    pub zacc: i16,
}

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Available on crate feature cubepilot only.

id: 90 Sent from simulation to autopilot. This packet is useful for high throughput applications such as hardware in the loop simulations.

Fields

time_usec: u64

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

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.

roll: f32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Roll angle

pitch: f32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Pitch angle

yaw: f32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Yaw angle

rollspeed: f32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Body frame roll / phi angular speed

pitchspeed: f32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Body frame pitch / theta angular speed

yawspeed: f32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Body frame yaw / psi angular speed

lat: i32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Latitude

lon: i32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Longitude

alt: i32

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Altitude

vx: i16

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Ground X Speed (Latitude)

vy: i16

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Ground Y Speed (Longitude)

vz: i16

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Ground Z Speed (Altitude)

xacc: i16

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

X acceleration

yacc: i16

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Y acceleration

zacc: i16

👎Deprecated: Suffers from missing airspeed fields and singularities due to Euler angles. See HIL_STATE_QUATERNION (Deprecated since 2013-07)

Z acceleration

Implementations

impl HIL_STATE_DATA

pub const ENCODED_LEN: usize = 56usize

pub const DEFAULT: Self

Trait Implementations

impl Clone for HIL_STATE_DATA

fn clone(&self) -> HIL_STATE_DATA

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Debug for HIL_STATE_DATA

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

Formats the value using the given formatter.

impl Default for HIL_STATE_DATA

fn default() -> Self

Returns the “default value” for a type.

impl<'de> Deserialize<'de> for HIL_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 HIL_STATE_DATA

const ID: u32 = 90u32

const NAME: &'static str = "HIL_STATE"

const EXTRA_CRC: u8 = 183u8

const ENCODED_LEN: usize = 56usize

type Message = MavMessage

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

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

impl PartialEq for HIL_STATE_DATA

fn eq(&self, other: &HIL_STATE_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 HIL_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 HIL_STATE_DATA