shinespark/src/fighter/state/air.rs

use crate::fighter::state::land::{LandingState, LandingType};
use crate::fighter::state::{CollisionContext, FighterState};
use crate::fighter::*;
use crate::input::FighterCommands;

#[derive(Default, Debug, Clone, Copy, Hash)]
pub struct AirborneStateCommon {
    pub is_fast_falling: bool,
}

pub fn process_fast_fall(
    airborne_state_common: &mut AirborneStateCommon,
    input: &mut FighterInput,
    velocity: &mut FighterVelocity,
    attributes: &FighterAttributes,
) {
    if velocity.y.is_negative() {
        if input.has_command(FighterCommands::SmashMoveDown) {
            airborne_state_common.is_fast_falling = true;
        }
        input.clear_command(FighterCommands::SmashMoveDown);
    }

    if airborne_state_common.is_fast_falling {
        velocity.y = -attributes.fast_fall_speed;
    }
}

pub fn integrate_gravity(
    velocity: &mut FighterVelocity,
    attributes: &FighterAttributes,
    fast_fall: bool,
) {
    velocity.y -= attributes.gravity;

    let terminal_vel = if fast_fall {
        -attributes.fast_fall_speed
    } else {
        -attributes.terminal_velocity
    };
    velocity.y = velocity.y.max(terminal_vel);
}

pub fn apply_air_drift(
    velocity: &mut FighterVelocity,
    attribs: &FighterAttributes,
    input: &FighterInput,
) {
    if input.get_last_frame().movement.x.is_zero() {
        if velocity.x.abs() < attribs.air_friction {
            velocity.x = FGi32::ZERO;
        } else {
            let velocity_sign = velocity.x.signum();
            velocity.x += (-velocity_sign) * attribs.air_friction;
        }
    } else {
        let target_velocity = input.get_last_frame().movement.x * attribs.air_drift_max;
        let mut acceleration = input.get_last_frame().movement.x.signum()
            * attribs.air_acceleration_base
            + input.get_last_frame().movement.x * attribs.air_acceleration_stick;

        // Acceleration opposes velocity
        if acceleration * velocity.x < 0 {
            // do nothing
        } else {
            let predicted_vel = velocity.x + acceleration;
            let will_go_past = predicted_vel.abs() > target_velocity.abs();

            if velocity.x.abs() < target_velocity.abs() && will_go_past {
                // Prevent overshoot
                acceleration = target_velocity - velocity.x
            } else if velocity.x.abs() > target_velocity.abs() {
                let diff = (velocity.x - target_velocity).abs();
                acceleration = velocity.x.signum() * (-(attribs.air_friction).min(diff));
            }
        }

        velocity.x += acceleration;
    }
}

pub fn apply_air_motion(
    velocity: &FighterVelocity,
    translation: &mut FighterTranslation,
    prev_translation: &mut FighterPreviousTranslation,
) {
    // Vertical velocity should be 0 on the ground
    prev_translation.0 = translation.0;
    translation.0 += velocity.0;
}

pub fn update_standard_motion(
    ctx: &mut crate::fighter::state::UpdateContext,
    airborne_common: &mut AirborneStateCommon,
) {
    process_fast_fall(
        airborne_common,
        ctx.input,
        &mut ctx.velocity,
        ctx.fighter_attributes,
    );
    integrate_gravity(
        ctx.velocity,
        ctx.fighter_attributes,
        airborne_common.is_fast_falling,
    );
    apply_air_drift(ctx.velocity, ctx.fighter_attributes, ctx.input);
    apply_air_motion(
        ctx.velocity,
        ctx.translation,
        ctx.prev_translation,
    );
}

pub fn collision_interrupt(
    ctx: &mut CollisionContext,
    landing_type: LandingType,
) -> Option<FighterState> {
    let res = ctx.air_collide_with_stage()?;
    let diff = res.hit_position - ctx.translation.0;
    ctx.ecb.bottom -= diff;
    ctx.ecb.top -= diff;
    ctx.ecb.left -= diff;
    ctx.ecb.right -= diff;
    ctx.translation.0 = res.hit_position;
    ctx.presentation_snap.0 = true;
    ctx.surface.land(res.line_id);
    Some(FighterState::Land(LandingState::create(landing_type)))
}

#[cfg(test)]
mod tests {
    use super::*;
    use crate::{
        input::{FighterInput, FighterInputFrame},
        math::vec::FGVec2,
    };

    fn test_attributes() -> FighterAttributes {
        FighterAttributes {
            base_walk_accel: FGi32::ZERO,
            stick_walk_accel: FGi32::ZERO,
            max_walk_vel: FGi32::ZERO,
            dash_acceleration_duration: 0,
            dash_duration: 0,
            dash_initial_velocity: FGi32::ZERO,
            base_dash_accel: FGi32::ZERO,
            stick_dash_accel: FGi32::ZERO,
            max_dash_vel: FGi32::ZERO,
            jumpsquat_duration: 0,
            short_hop_vertical_velocity: FGi32::ZERO,
            full_jump_vertical_velocity: FGi32::ZERO,
            jump_horizontal_velocity: FGi32::ZERO,
            air_jump_multiplier: FGi32::ZERO,
            air_jump_horizontal_velocity: FGi32::ZERO,
            landing_iasa: 0,
            landing_duration: 0,
            air_acceleration_base: FGi32::ZERO,
            air_acceleration_stick: FGi32::ZERO,
            max_air_horizontal_velocity: FGi32::lit("1.2"),
            air_drift_max: FGi32::lit("1.2"),
            ground_friction: FGi32::ZERO,
            terminal_velocity: FGi32::ZERO,
            fast_fall_speed: FGi32::ZERO,
            gravity: FGi32::ZERO,
            weight: FGi32::lit("1"),
            air_friction: FGi32::lit("0.001"),
            air_dodge_duration: 0,
            air_dodge_velocity: FGi32::ZERO,
            air_dodge_decay: FGi32::ZERO,
        }
    }

    #[test]
    fn zero_air_acceleration_is_symmetric() {
        let attributes = test_attributes();
        let mut right_input = FighterInput::default();
        right_input.push_input_frame(FighterInputFrame {
            movement: FGVec2::new(FGi32::ONE, FGi32::ZERO),
            ..default()
        });
        let mut left_input = FighterInput::default();
        left_input.push_input_frame(FighterInputFrame {
            movement: FGVec2::new(-FGi32::ONE, FGi32::ZERO),
            ..default()
        });

        let mut right_velocity = FighterVelocity(FGVec2::ZERO);
        let mut left_velocity = FighterVelocity(FGVec2::ZERO);
        apply_air_drift(&mut right_velocity, &attributes, &right_input);
        apply_air_drift(&mut left_velocity, &attributes, &left_input);

        assert_eq!(right_velocity.x, FGi32::ZERO);
        assert_eq!(left_velocity.x, FGi32::ZERO);
    }
}