115 lines
4.4 KiB
C
115 lines
4.4 KiB
C
/*
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* Copyright (C) 2023 Daniele Lacamera <root@danielinux.net>
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*
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* This program is free software: you can redistribute it and/or modify
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* it under the terms of the GNU Lesser General Public License as published by
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* the Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* This program is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU Lesser General Public License for more details.
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*
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* You should have received a copy of the GNU Lesser General Public License
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* along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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#ifndef KSP_SERIAL_H
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#define KSP_SERIAL_H
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#include <stdint.h>
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typedef struct __attribute__((packed)) vesselData {
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uint8_t id; //1
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float AP; //2
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float PE; //3
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float SemiMajorAxis; //4
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float SemiMinorAxis; //5
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float VVI; //6
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float e; //7
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float inc; //8
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float G; //9
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int32_t TAp; //10
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int32_t TPe; //11
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float TrueAnomaly; //12
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float Density; //13
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int32_t period; //14
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float RAlt; //15
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float Alt; //16
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float Vsurf; //17
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float Lat; //18
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float Lon; //19
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float LiquidFuelTot; //20
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float LiquidFuel; //21
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float OxidizerTot; //22
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float Oxidizer; //23
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float EChargeTot; //24
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float ECharge; //25
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float MonoPropTot; //26
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float MonoProp; //27
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float IntakeAirTot; //28
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float IntakeAir; //29
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float SolidFuelTot; //30
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float SolidFuel; //31
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float XenonGasTot; //32
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float XenonGas; //33
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float LiquidFuelTotS; //34
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float LiquidFuelS; //35
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float OxidizerTotS; //36
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float OxidizerS; //37
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uint32_t MissionTime; //38
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float deltaTime; //39
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float VOrbit; //40
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uint32_t MNTime; //41
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float MNDeltaV; //42
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float Pitch; //43
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float Roll; //44
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float Heading; //45
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uint16_t ActionGroups; //46 status bit order:SAS, RCS, Light, Gear, Brakes, Abort, Custom01 - 10
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uint8_t SOINumber; //47 SOI Number (decimal format: sun-planet-moon e.g. 130 = kerbin, 131 = mun)
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uint8_t MaxOverHeat; //48 Max part overheat (% percent)
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float MachNumber; //49
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float IAS; //50 Indicated Air Speed
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uint8_t CurrentStage; //51 Current stage number
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uint8_t TotalStage; //52 TotalNumber of stages
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float TargetDist; //53 Distance to targeted vessel (m)
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float TargetV; //54 Target vessel relative velocity (m/s)
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uint8_t NavballSASMode; //55 Combined byte for navball target mode and SAS mode
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// First four bits indicate AutoPilot mode:
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// 0 SAS is off //1 = Regular Stability Assist //2 = Prograde
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// 3 = RetroGrade //4 = Normal //5 = Antinormal //6 = Radial In
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// 7 = Radial Out //8 = Target //9 = Anti-Target //10 = Maneuver node
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// Last 4 bits set navball mode. (0=ignore,1=ORBIT,2=SURFACE,3=TARGET)
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} vesselData_t;
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typedef struct __attribute__((packed)) handShakePacket {
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uint8_t id;
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uint8_t M1;
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uint8_t M2;
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uint8_t M3;
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} handShakePacket_t;
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typedef struct __attribute__((packed)) controlPacket {
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uint8_t id;
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uint8_t MainControls; // SAS RCS Lights Gear Brakes Precision Abort Stage
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uint8_t Mode; // 0 = stage, 1 = docking, 2 = map
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uint16_t ControlGroup; // control groups 1-10 in 2 bytes
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uint8_t NavBallSASMode; // other stuff
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uint8_t AdditionalControlByte1;
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int16_t Pitch; // -1000 -> 1000
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int16_t Roll; // -1000 -> 1000
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int16_t Yaw; // -1000 -> 1000
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int16_t TX; // -1000 -> 1000
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int16_t TY; // -1000 -> 1000
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int16_t TZ; // -1000 -> 1000
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int16_t WheelSteer; // -1000 -> 1000
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int16_t Throttle; // 0 -> 1000
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int16_t WheelThrottle; // 0 -> 1000
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} controlPacket_t;
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extern vesselData_t *cur_vdata;
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void ksp_serial_send(const void *data, uint8_t len);
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#endif
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