Struct ControlInput 

pub struct ControlInput {
    pub thrust_direction: Vec3,
    pub steering_acceleration_mps2: Vec3,
}

World-frame controls held constant for one caller-requested simulation step.

Fields

thrust_direction: Vec3

Nonzero thrust-axis vector. The solver normalizes it before applying thrust. This is an externally supplied orientation, not an instantaneous attitude solver.

steering_acceleration_mps2: Vec3

Additional acceleration requested by an external steering/actuator model. Its magnitude is capped by crate::IntegratorSettings::max_steering_accel_mps2. It can act during coast, allowing callers to model fins or other control authority.

Implementations

impl ControlInput

pub fn along(thrust_direction: Vec3) -> Self

Specify a thrust axis with no additional steering acceleration. Inputs are validated when the simulator steps.

Trait Implementations

impl Clone for ControlInput

fn clone(&self) -> Self

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Copy for ControlInput

impl Debug for ControlInput

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

Formats the value using the given formatter.

impl Default for ControlInput

fn default() -> Self

Returns the “default value” for a type.

impl PartialEq for ControlInput

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

Equality operator ==.

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

Inequality operator !=.

impl StructuralPartialEq for ControlInput