130 lines
3.9 KiB
C
130 lines
3.9 KiB
C
#pragma once
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#ifndef __INTELLISENSE__
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# define MODULE_EXPORT __attribute__( ( visibility( "default" ) ) )
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# define MODULE_WASM_MODNAME(mod) __attribute__((import_module(mod)))
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#else
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# define MODULE_EXPORT
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# define MODULE_WASM_MODNAME(mod)
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# define __attribute__(x)
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# define __restrict__
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#endif
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/******************************** Constants ********************************/
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// 190lbs default
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#define PILOT_WEIGHT(IS_IMPERIAL) ((IS_IMPERIAL) ? (190.0) : (86.0))
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// 200lbs per tank (one LD3)
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#define AUX_WEIGHT(IS_IMPERIAL) ((IS_IMPERIAL) ? (200.0) : (91.0))
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//PMC pallet due to 104in door
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#define MAX_FRONT_CARGO(IS_IMPERIAL) ((IS_IMPERIAL) ? (6.0 * 15000.0) : (6.0 * 6804.0))
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//LD3s due to 70in door, ER option takes up two slots
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#define MAX_REAR_CARGO(IS_IMPERIAL, IS_ER) ((IS_IMPERIAL) ? ((IS_ER ? 12.0 : 14.0) * 3500.0) : ((IS_ER ? 12.0 : 14.0) * 1588.0))
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// Max TOW
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#define MAX_TOW(IS_IMPERIAL) ((IS_IMPERIAL) ? (625500) : (283722))
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#define MAX_TOW_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (630500) : (285990))
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// Max Fuel
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#define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213))
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#define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193))
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// Arms Shared
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#define ARM_EMPTY -159.6
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#define ARM_PILOT 984.0
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#define ARM_FIRST_OFFICER 984.0
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#define ARM_ENGINEER 960.0
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#define ARM_FORWARD_CARGO 360.0
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#define ARM_REAR_CARGO -360.0
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#define ARM_LEFT_AUX 60.0
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#define ARM_RIGHT_AUX 60.0
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// Arms Fuel
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#define ARM_MAIN1 -240.0
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#define ARM_MAIN3 -240.0
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#define ARM_MAIN2 120.0
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#define ARM_UPPER_AUX 0.0
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#define ARM_LOWER_AUX 0.0
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#define ARM_MAIN1_TIP -468.0
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#define ARM_MAIN3_TIP -468.0
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#define ARM_TAIL -840.0
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#define ARM_FORWARD_AUX1 60.0
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#define ARM_FORWARD_AUX2 60.0
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// MAC
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#define ROOT_CHORD 34.68
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#define WING_SPAN 170.5
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#define WING_AREA 3648.0
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#define QUARTER_MAC -165.0 //aero_center
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#define TIP_CHORD ((2.0 * WING_AREA) / WING_SPAN - ROOT_CHORD)
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#define TAPER_RATIO (TIP_CHORD / ROOT_CHORD)
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#define MAC ((2.0 / 3.0) * ROOT_CHORD * ((1.0 + TAPER_RATIO + (TAPER_RATIO * TAPER_RATIO)) / (1.0 + TAPER_RATIO)) * 12.0)
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#define LEMAC (QUARTER_MAC + (1.0 / 4.0) * MAC)
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// CG Limits
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#define MIN_CG 12.0
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#define MAX_CG 34.0
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#define CG_TOLERANCE 0.05
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// GSX States
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#define GSX_SERVICE_ACTIVE 5
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/********************************* Macros **********************************/
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// Conversions
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#define TO_POUNDS(IS_IMPERIAL, VALUE) ((IS_IMPERIAL) ? (VALUE) : (VALUE) * 2.20462262185)
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#define FROM_POUNDS(IS_IMPERIAL, VALUE) ((IS_IMPERIAL) ? (VALUE) : (VALUE) * (1.0 / 2.20462262185))
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// MAC
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#define TO_PERCENT_MAC(POS) ((((POS) - LEMAC) / MAC) * -100.0)
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/********************************** ENUMS **********************************/
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enum DATA_DEFINITIONS {
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DATA_DEFINITION_EMPTY_WEIGHT,
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DATA_DEFINITION_PAYLOAD_PAX,
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DATA_DEFINITION_PAYLOAD_F,
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DATA_DEFINITION_FUEL,
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DATA_DEFINITION_GSX,
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DATA_DEFINITION_USER_DATA,
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};
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enum DATA_REQUESTS {
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DATA_REQUEST_EMPTY_WEIGHT,
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DATA_REQUEST_PAYLOAD_PAX,
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DATA_REQUEST_PAYLOAD_F,
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DATA_REQUEST_FUEL,
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DATA_REQUEST_GSX,
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DATA_REQUEST_USER_DATA,
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};
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/***************************** Data structures *****************************/
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typedef struct {
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double isCargo;
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double isER;
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double isImperial;
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} UserData_t;
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typedef struct {
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double boardingState; // See manual, 5 => active
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double deboardingState; // See manual, 5 => active
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double passengersBoarded; // Num pax
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double passengersDeboarded; // Num pax
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double cargoBoarded; // In percent
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double cargoDeboarded; // In percent
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} GSXData_t;
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typedef struct {
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// SimConnect mapped
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double poundsPerGallon; // DO NOT USE
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double main1;
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double main3;
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double main2;
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double upperAux;
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double lowerAux;
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double main1Tip;
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double main3Tip;
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double tail;
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double forwardAux1;
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double forwardAux2;
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// Additional properties
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double total;
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} FuelData_t;
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typedef struct {
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bool GSXSync;
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double paxWeightKG;
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double bagWeightKG;
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double paxWeightLBS;
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double bagWeightLBS;
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} UserOptions_t; |