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https://github.com/deater/dos33fsprogs.git
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ksp: have BASIC physics going
This commit is contained in:
Vince Weaver
parent
e5f2c1de1a
commit
4e74910bfc
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@ -15,6 +15,9 @@ LAUNCH.BAS: launch.bas
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LOADING.BAS: loading.bas
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$(TXT2BAS) < loading.bas > LOADING.BAS
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PHYSICS.BAS: physics.bas
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$(TXT2BAS) < physics.bas > PHYSICS.BAS
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VAB.BAS: vab.bas
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$(TXT2BAS) < vab.bas > VAB.BAS
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@ -23,6 +26,7 @@ VAB.BAS: vab.bas
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ksp.dsk: ACMPLX.BAS \
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LAUNCH.BAS \
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LOADING.BAS LOADING.HGR SQUAD.HGR TITLE.HGR \
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PHYSICS.BAS \
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VAB.BAS VAB.HGR
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$(DOS33) -y ksp.dsk SAVE B LOADING.HGR
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$(DOS33) -y ksp.dsk SAVE B SQUAD.HGR
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@ -32,6 +36,7 @@ ksp.dsk: ACMPLX.BAS \
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$(DOS33) -y ksp.dsk SAVE A LOADING.BAS
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$(DOS33) -y ksp.dsk SAVE A ACMPLX.BAS
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$(DOS33) -y ksp.dsk SAVE A LAUNCH.BAS
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$(DOS33) -y ksp.dsk SAVE A PHYSICS.BAS
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LOADING.HGR: loading.pcx
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@ -120,9 +120,10 @@ int main(int argc, char **argv) {
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while(1) {
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/* 4010 */
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fuel_left=fuel_mass*100.0/total_fuel;
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thrusting=autopilot(fuel_left, rocket_altitude,&angle);
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thrusting=1;//autopilot(fuel_left, rocket_altitude,&angle);
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if (thrusting) {
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if (fuel_mass<0.1) {
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@ -144,12 +145,15 @@ int main(int argc, char **argv) {
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rocket_acceleration_y=0.0;
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}
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if (rocket_y<0) gravity_angle=PI+atan(rocket_x/rocket_y);
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else gravity_angle=atan(rocket_x/rocket_y);
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/* 4060 */
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gravity_angle=atan(rocket_x/rocket_y);
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if (rocket_y<0) gravity_angle+=PI;
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/* 4070 */
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gravity_y=cos(gravity_angle)*gravity;
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gravity_x=sin(gravity_angle)*gravity;
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/* 4080 */
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rocket_acceleration_y+=gravity_y;
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rocket_acceleration_x+=gravity_x;
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@ -168,6 +172,8 @@ int main(int argc, char **argv) {
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rocket_altitude=vector_magnitude(rocket_x,rocket_y);
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/* 5020 */
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if (rocket_altitude<KERBIN_RADIUS) {
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if (rocket_velocity<20.0) {
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printf("LANDED!\n");
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@ -178,6 +184,7 @@ int main(int argc, char **argv) {
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break;
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}
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/* 5030 */
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/* Adjust gravity */
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gravity=-9.8/(
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((rocket_altitude)/KERBIN_RADIUS)*
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@ -188,13 +195,14 @@ int main(int argc, char **argv) {
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htabvtab(1,21);
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printf("Time: %lf\n",time);
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printf("ALT: %lf m\tg=%lf\n",rocket_altitude-KERBIN_RADIUS,gravity);
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printf("ALT: %lf km\tg=%lf\n",(rocket_altitude-KERBIN_RADIUS)/1000.0,
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gravity);
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printf("VEL: %lf m/s\tStage: %d\n",
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rocket_velocity,
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stage);
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printf("ACCEL: %lf g\tFuel: %lf%%",
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vector_magnitude(rocket_acceleration_x,rocket_acceleration_y)/9.8,
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fuel_mass*100.0/total_fuel);
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fuel_left);
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htabvtab(30,21);
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printf("ZURGTROYD");
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@ -212,8 +220,9 @@ int main(int argc, char **argv) {
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printf("x=%lf y=%lf\n",rocket_x,rocket_y);
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htabvtab(20,11);
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printf("vx=%lf vy=%lf\n",rocket_velocity_x,
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rocket_velocity_y);
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printf("vx=%lf vy=%lf ax=%lf ay=%lf\n",
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rocket_velocity_x,rocket_velocity_y,
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rocket_acceleration_x,rocket_acceleration_y);
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htabvtab(20,10);
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printf("angle=%lf\n",angle);
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69
ksp/physics.bas
Normal file
69
ksp/physics.bas
Normal file
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@ -0,0 +1,69 @@
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3000 AN=0.785
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3001 CM=1
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3002 E=3
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3003 EI=270
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3004 EM=1.5*E
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3005 ET=168*E
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3006 T=6
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3007 KM=0.5*T
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3008 FM=4.0*T
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3009 TF=FM
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3010 FL=100
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3011 G=-9.8
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3012 GX=0:GY=-9.8:GA=0
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3013 V=0:VX=0:VY=0
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3014 AX=0:AY=0
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3015 KR=600000
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3016 RX=0:RY=KR+10
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3017 RA=KR
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3018 S=1:TH=1:T=0
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3020 TM=EM+KM+FM+CM
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3021 MT=TM-FM
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3022 DV=EI*G*LOG(TM/MT)
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3025 TW=ET/(TM*-G)
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3030 FR=ET/(EI*-G)
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3035 PRINT "DELTAV=";DV
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3040 PRINT "THRUST/WEIGHT=";TW
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3050 PRINT "FUEL FLOW RATE=";FR
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4000 REM
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4010 FL=FM*100/TF
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4020 IF TH<>1 THEN GOTO 4050
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4025 IF FM<0.1 THEN FM=0:AX=0:AY=0:GOTO 4050
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4030 AX=(ET/TM)*SIN(AN)
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4035 AY=(ET/TM)*COS(AN)
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4037 PRINT "ET=";ET;" TM=";TM
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4040 FM=FM-FR
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4045 TM=EM+KM+FM+CM
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4047 GOTO 4060
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4050 REM NOT THRUSTING
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4055 AX=0:AY=0
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4060 GA=ATN(RX/RY)
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4062 PRINT "GA=";GA;" AY=";AY
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4065 IF RY<0 THEN GA=GA+3.14
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4070 GY=COS(GA)*G
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4075 GX=SIN(GA)*G
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4080 AY=AY+GY
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4085 AX=AX+GX
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4090 ZX=VX
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4095 ZY=VY
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5000 VY=ZY+AY
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5005 VX=ZX+AX
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5010 V=SQR(VX*VX+VY*VY)
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5012 RY=RY+0.5*(ZY+VY)
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5014 RX=RX+0.5*(ZX+VX)
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5018 RA=SQR(RX*RX+RY*RY)
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5020 IF RA<KR THEN PRINT "CRASH": END
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5030 G=-9.8/((RA/KR)*(RA/KR))
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5035 PRINT "-------------------------"
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5040 PRINT "TIME: ";T
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5050 PRINT "ALT: ";(RA-KR)/1000;"KM","G ";G
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5060 PRINT "VEL: ";V;"M/S","STAGE: ";S
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5070 PRINT "ACCEL: ","FUEL: ";INT(FL);"%"
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5080 PRINT "GRAVANGLE ";GA*180/3.14
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5090 PRINT "X: ";RX;" Y: ";RY
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5100 PRINT "VX: ";VX;" VY: ";VY
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5110 PRINT "ANGLE: ";AN
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5112 PRINT "AX: ";AX;"AY: ";AY
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5118 T=T+1
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5120 REM GET A$:IF A$="Q" THEN END
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5130 GOTO 4000
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