implement tidal locking of moons
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parent
8a35eb350a
commit
d98b216c8d
16
src/cmd.rs
16
src/cmd.rs
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@ -91,6 +91,7 @@ struct ParserState {
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is_moon: bool,
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is_planet: bool,
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is_point_of_interest: bool,
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is_tidally_locked: bool,
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orbit_distance: Option<f64>,
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orbit_object_id: Option<String>,
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orbit_phase: Option<f64>,
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@ -149,6 +150,7 @@ impl Default for ParserState {
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is_moon: false,
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is_planet: false,
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is_point_of_interest: false,
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is_tidally_locked: false,
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orbit_distance: None,
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orbit_object_id: None,
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orbit_phase: None,
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@ -456,6 +458,9 @@ pub fn load_defs(mut ew_spawn: EventWriter<SpawnEvent>) {
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["ring", "yes"] => {
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state.has_ring = true;
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}
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["tidally", "locked"] => {
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state.is_tidally_locked = true;
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}
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["pointofinterest", "yes"] => {
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state.is_point_of_interest = true;
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}
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@ -848,6 +853,17 @@ fn spawn_entities(
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None
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};
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absolute_pos += nature::pos_offset_for_orbiting_body(r, mass, state.orbit_phase);
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if state.is_tidally_locked {
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if let Some(mass) = mass {
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rotation =
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Quat::from_rotation_y(nature::rotation_for_orbiting_body(r, mass) as f32);
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} else {
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error!("Attempted to use 'tidally locked' without specifying mass via 'orbitaround'");
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}
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}
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} else if state.is_tidally_locked {
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error!("Attempted to use 'tidally locked' without specifying orbital distance via 'orbitaround'");
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}
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let scale = Vec3::splat(
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if state.is_sun {
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@ -127,10 +127,11 @@ actor 0 0 0
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relativeto jupiter
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id thebe
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orbitaround jupiter 221900e3
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tidally locked
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scale 50e3
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moon yes
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collider handcrafted
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angularmomentum 0 0.0 0
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angularmomentum 0 0 0
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actor 0 0 0 orbitring
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relativeto jupiter
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scale 221900e3
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@ -230,3 +230,18 @@ pub fn pos_offset_for_orbiting_body(
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}
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return phase_dist_to_coords(-phase_radians, r);
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}
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/// Assumes the "front" (as seen in blender) is pointing at the orbited mass
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pub fn rotation_for_orbiting_body(
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orbit_distance: f64,
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mass: f64,
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) -> f64 {
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if let Ok(epoch) = SystemTime::now().duration_since(SystemTime::UNIX_EPOCH) {
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let orbital_period = nature::simple_orbital_period(mass, orbit_distance);
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let now = epoch.as_secs_f64() + ORBIT_TIME_OFFSET;
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PI * 2.0 * (now % orbital_period) / orbital_period - PI * 0.5
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} else {
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eprintln!("WARNING: Can't determine current time in calculate_position_offset_for_orbiting_body().");
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0.0
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}
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}
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