Revert "[MIRROR] /atom New() => Initialize() [MDB IGNORE]"

This commit is contained in:
Novacat
2022-08-27 08:49:56 -04:00
committed by GitHub
parent 0be7af4774
commit 1aa4c73e8d
599 changed files with 3329 additions and 4983 deletions
@@ -7,17 +7,6 @@ somewhere on that shuttle. Subtypes of these can be then used to perform ship ov
var/obj/effect/overmap/visitable/ship/linked
var/list/viewers // Weakrefs to mobs in direct-view mode.
var/extra_view = 0 // how much the view is increased by when the mob is in overmap mode.
var/list/whitelisted_types = list(/obj/effect/overmap/visitable/ship)
var/list/blacklisted_types = list()
/obj/machinery/computer/ship/Initialize()
. = ..()
var/list/L = list()
for(var/type in whitelisted_types)
L |= typesof(type)
for(var/type in blacklisted_types)
L -= typesof(type)
whitelisted_types = L
// A late init operation called in SSshuttles, used to attach the thing to the right ship.
/obj/machinery/computer/ship/proc/attempt_hook_up(obj/effect/overmap/visitable/ship/sector)
@@ -189,13 +189,11 @@
light_color = "#ed9200"
anchored = TRUE
/obj/effect/engine_exhaust/Initialize(var/ml, var/ndir, var/flame)
. = ..(ml)
/obj/effect/engine_exhaust/New(var/turf/nloc, var/ndir, var/flame)
..(nloc)
if(flame)
icon_state = "exhaust"
if(isturf(loc))
var/turf/T = loc
T.hotspot_expose(1000,125)
nloc.hotspot_expose(1000,125)
set_light(0.5, 3)
set_dir(ndir)
QDEL_IN(src, 20)
@@ -1,97 +0,0 @@
//Thermal nozzle engine
/datum/ship_engine/thermal
name = "thermal engine"
/datum/ship_engine/thermal/get_status()
..()
var/obj/machinery/atmospherics/unary/engine/E = engine
return "Fuel pressure: [E.air_contents.return_pressure()]"
/datum/ship_engine/thermal/get_thrust()
..()
var/obj/machinery/atmospherics/unary/engine/E = engine
if(!is_on())
return 0
var/pressurized_coef = E.air_contents.return_pressure()/E.effective_pressure
return round(E.thrust_limit * E.nominal_thrust * pressurized_coef)
/datum/ship_engine/thermal/burn()
..()
var/obj/machinery/atmospherics/unary/engine/E = engine
return E.burn()
/datum/ship_engine/thermal/set_thrust_limit(var/new_limit)
..()
var/obj/machinery/atmospherics/unary/engine/E = engine
E.thrust_limit = new_limit
/datum/ship_engine/thermal/get_thrust_limit()
..()
var/obj/machinery/atmospherics/unary/engine/E = engine
return E.thrust_limit
/datum/ship_engine/thermal/is_on()
..()
var/obj/machinery/atmospherics/unary/engine/E = engine
return E.on
/datum/ship_engine/thermal/toggle()
..()
var/obj/machinery/atmospherics/unary/engine/E = engine
E.on = !E.on
//Actual thermal nozzle engine object
/obj/machinery/atmospherics/unary/engine
name = "engine nozzle"
desc = "Simple thermal nozzle, uses heated gast to propell the ship."
icon = 'icons/obj/ship_engine.dmi'
icon_state = "nozzle"
var/on = 1
var/thrust_limit = 1 //Value between 1 and 0 to limit the resulting thrust
var/nominal_thrust = 3000
var/effective_pressure = 3000
var/datum/ship_engine/thermal/controller
/obj/machinery/atmospherics/unary/engine/Initialize()
. = ..()
controller = new(src)
/obj/machinery/atmospherics/unary/engine/Destroy()
..()
controller.die()
/obj/machinery/atmospherics/unary/engine/proc/burn()
if (!on)
return
if(air_contents.temperature > 0)
var/transfer_moles = 100 * air_contents.volume/max(air_contents.temperature * R_IDEAL_GAS_EQUATION, 0,01)
transfer_moles = round(thrust_limit * transfer_moles, 0.01)
if(transfer_moles > air_contents.total_moles)
on = !on
return 0
var/datum/gas_mixture/removed = air_contents.remove(transfer_moles)
loc.assume_air(removed)
if(air_contents.temperature > PHORON_MINIMUM_BURN_TEMPERATURE)
var/exhaust_dir = reverse_direction(dir)
var/turf/T = get_step(src,exhaust_dir)
if(T)
new/obj/effect/engine_exhaust(T,exhaust_dir,air_contents.temperature)
return 1
//Exhaust effect
/obj/effect/engine_exhaust
name = "engine exhaust"
icon = 'icons/effects/effects.dmi'
icon_state = "exhaust"
anchored = 1
/obj/effect/engine_exhaust/Initialize(var/ml, var/ndir, var/temp)
set_dir(ndir)
. = ..()
if(isturf(loc))
var/turf/nloc = turf
nloc.hotspot_expose(temp,125)
QDEL_IN(2 SECONDS)