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Add experimental vertical flightplan phases, allow user to set cruise flight level in descent phase

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legoboyvdlp R 2020-04-16 13:25:06 +01:00 • committed by Jonathan Redpath
parent e4182ae9b8
commit 5417101ca0
3 changed files with 51 additions and 30 deletions
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68
Nasal/FMGC/FMGC.nas
View file

@ -37,7 +37,7 @@ var wowr = 0;
var targetalt = 0;
var targetvs = 0;
var targetfpa = 0;
var reduc_agl_ft = 0;
var accel_agl_ft = 0;
var locarm = 0;
var apprarm = 0;
var gear0 = 0;
@ -95,6 +95,8 @@ var newvert = 0;
var newvertarm = 0;
var thr1 = 0;
var thr2 = 0;
var altsel = 0;
var crzFl = 0;
setprop("FMGC/internal/maxspeed", 0);
setprop("FMGC/internal/minspeed", 0);
setprop("position/gear-agl-ft", 0);
@ -127,6 +129,7 @@ var FMGCinit = func {
setprop("FMGC/internal/decel", 0);
setprop("FMGC/internal/loc-source", "NAV0");
setprop("FMGC/internal/optalt", 0);
setprop("FMGC/internal/landing-time", -99);
masterFMGC.start();
various.start();
various2.start();
@ -193,7 +196,7 @@ var masterFMGC = maketimer(0.2, func {
targetalt = getprop("it-autoflight/internal/alt");
targetvs = getprop("it-autoflight/input/vs");
targetfpa = getprop("it-autoflight/input/fpa");
reduc_agl_ft = getprop("it-autoflight/settings/accel-agl-ft");
accel_agl_ft = getprop("it-autoflight/settings/accel-agl-ft");
locarm = getprop("it-autopilot/output/loc-armed");
apprarm = getprop("it-autopilot/output/appr-armed");
gear0 = getprop("gear/gear[0]/wow");
@ -210,71 +213,65 @@ var masterFMGC = maketimer(0.2, func {
gear0 = getprop("gear/gear[0]/wow");
state1 = getprop("systems/thrust/state1");
state2 = getprop("systems/thrust/state2");
altSel = getprop("it-autoflight/input/alt");
crzFl = getprop("FMGC/internal/cruise-fl");
if (getprop("gear/gear[0]/wow") != getprop("gear/gear[0]/wow-fmgc")) {
setprop("gear/gear[0]/wow-fmgc", getprop("gear/gear[0]/wow"));
}
if ((n1_left < 70 or n1_right < 70) and gs < 90 and mode == " " and gear0 == 1 and phase == 1) {
if ((n1_left < 85 or n1_right < 85) and gs < 90 and mode == " " and gear0 == 1 and phase == 1) { # rejected takeoff
setprop("FMGC/status/phase", 0);
setprop("systems/pressurization/mode", "GN");
}
if (gear0 == 1 and phase == 0 and ((n1_left >= 70 and n1_right >= 70) or gs >= 90) and (state1 == "TOGA" or state2 == "TOGA") or (flx == 1 and (state1 == "MCT" or state2 == "MCT")) or (flx == 1 and ((state1 == "MAN THR" and thr1 >= 0.83) or
(state2 == "MAN THR" and thr2 >= 0.83)))) {
if (gear0 == 1 and phase == 0 and ((n1_left >= 85 and n1_right >= 85) or gs >= 90) and mode == "SRS") {
setprop("FMGC/status/phase", 1);
setprop("systems/pressurization/mode", "TO");
}
if (phase == 1 and ((mode != "SRS" and mode != " ") or alt >= reduc_agl_ft)) {
if (phase == 1 and ((mode != "SRS" and mode != " ") or alt >= accel_agl_ft)) {
setprop("FMGC/status/phase", 2);
setprop("systems/pressurization/mode", "TO");
}
if ((phase == 3 or phase == 4) and (mode == "OP CLB" or mode == "CLB" or (modeI == "V/S" and getprop("it-autoflight/input/vs") >= 100) or (modeI == "FPA" and getprop("it-autoflight/input/fpa") >= 0.1))) {
setprop("FMGC/status/phase", 2);
setprop("systems/pressurization/mode", "TO");
}
if ((phase == 2 or phase == 4) and (mode == "ALT" or mode == "ALT CRZ" or mode == "ALT CST")) {
if (phase == 2 and (mode == "ALT CRZ" or mode == "ALT CRZ*")) {
setprop("FMGC/status/phase", 3);
setprop("systems/pressurization/mode", "CR");
}
if ((phase == 2 or phase == 3) and (mode == "OP DES" or mode == "DES" or (modeI == "V/S" and getprop("it-autoflight/input/vs") <= -100) or (modeI == "FPA" and getprop("it-autoflight/input/fpa") <= -0.1))) {
if (crzFl >= 20000) {
if ((phase == 2 or phase == 3) and (flightPlanController.arrivalDist <= 200 or altSel < 20000)) {
setprop("FMGC/status/phase", 4);
setprop("systems/pressurization/mode", "DE");
}
} else {
if ((phase == 2 or phase == 3) and (flightPlanController.arrivalDist <= 200 or altSel < crzFl)) { # todo - not sure about crzFl condition, investigate what happens!
setprop("FMGC/status/phase", 4);
setprop("systems/pressurization/mode", "DE");
}
}
if (!wowl and !wowr and aglalt < 7200 and (phase == "4" or mode == "G/S" or mode == "LAND" or mode == "FLARE")) {
if (getprop("/FMGC/internal/decel")) {
setprop("FMGC/status/phase", 5);
}
if (flightPlanController.num[2].getValue() > 0 and getprop("/FMGC/flightplan[2]/active") == 1 and flightPlanController.arrivalDist <= 15) {
if (flightPlanController.num[2].getValue() > 0 and getprop("/FMGC/flightplan[2]/active") == 1 and flightPlanController.arrivalDist <= 15 and (modelat == "NAV" or modelat == "LOC" or modelat == "LOC*") and aglalt < 9500) { #todo decel pseudo waypoint
setprop("/FMGC/internal/decel", 1);
} else if (getprop("/FMGC/internal/decel") == 1 and (phase == 0 or phase == 6)) {
setprop("/FMGC/internal/decel", 0);
}
#handle go-around
if ((phase == "5" or phase == "7") and state1 == "TOGA" and state2 == "TOGA") {
if ((phase == "5") and state1 == "TOGA" and state2 == "TOGA") {
setprop("FMGC/status/phase", 6);
setprop("systems/pressurization/mode", "TO");
setprop("it-autoflight/input/toga", 1);
}
if (phase == "6" and alt >= reduc_agl_ft) {
if (phase == "6" and alt >= accel_agl_ft) { # todo when insert altn or new dest
setprop("FMGC/status/phase", 2);
}
if (wowl and wowr and (phase == "2" or phase == "3" or phase == "4" or phase == "5" or phase == "6")) {
setprop("FMGC/status/phase", 7);
}
if (wowl and wowr and gs <= 40 and phase == "7" and ap1 == 0 and ap2 == 0) {
reset_FMGC();
}
if (getprop("systems/navigation/adr/computation/overspeed-vfe-spd") != 1024) {
setprop("FMGC/internal/maxspeed", getprop("systems/navigation/adr/computation/overspeed-vfe-spd") - 4);
} elsif (pts.Gear.position[0].getValue() != 0 or pts.Gear.position[1].getValue() != 0 or pts.Gear.position[2].getValue() != 0) {
@ -752,3 +749,22 @@ var switchDatabase = func {
setprop("FMGC/internal/navdatabasecode", code2);
setprop("FMGC/internal/navdatabasecode2", code1);
}
setlistener("gear/gear[1]/wow", func() {
if (timer30secLandingstart.isRunning) {
timer30secLandingstart.stop();
}
if (getprop("gear/gear[1]/wow") == 1 and getprop("FMGC/internal/landing-time") == -99) {
timer30secLandingstart();
setprop("FMGC/internal/landing-time", pts.Sim.Time.elapsedSec.getValue());
}
}, 0, 0);
var timer30secLandingstart = maketimer(0.1, func() {
if (pts.Sim.Time.elapsedSec.getValue() > getprop("FMGC/internal/landing-time") + 30) {
setprop("FMGC/status/phase", 7);
setprop("FMGC/internal/landing-time", -99);
timer30secLandingstart.stop();
}
});

5
Nasal/MCDU/MCDU.nas
View file

@ -674,8 +674,13 @@ var pagebutton = func(btn, i) {
setprop("MCDU[" ~ i ~ "]/page", "PERFAPPR");
} else if (getprop("FMGC/status/phase") == 6) {
setprop("MCDU[" ~ i ~ "]/page", "PERFGA");
} else if (getprop("FMGC/status/phase") == 7) {
reset_FMGC();
}
} else if (btn == "init") {
if (getprop("FMGC/status/phase") == 7) {
reset_FMGC();
}
setprop("MCDU[" ~ i ~ "]/page", "INITA");
} else if (btn == "data") {
setprop("MCDU[" ~ i ~ "]/page", "DATA");

2
Nasal/MCDU/PROGDES.nas
View file

@ -16,7 +16,7 @@ var progDESInput = func(key, i) {
if (crzs >= 1 and crzs <= 3 and scratchpad > 0 and scratchpad <= 430 and altSet.getValue() <= scratchpad * 100) {
setprop("FMGC/internal/cruise-fl-prog", scratchpad);
setprop("MCDU[" ~ i ~ "]/scratchpad", "");
if (getprop("FMGC/status/phase") == 5 or getprop("FMGC/status/phase") == 6) {
if (getprop("FMGC/status/phase") == 4 or getprop("FMGC/status/phase") == 5 or getprop("FMGC/status/phase") == 6) {
setprop("FMGC/status/phase", 3);
setprop("FMGC/internal/activate-once", 0);
setprop("FMGC/internal/activate-twice", 0);