change per-aircraft configuration to a single function object that is
registered with dynamic_view.register() and is called in the main loop, replacing the default plane/helicopter function. This has access to all class functions/members and sets me.heading_offset, me.pitch_offset, and me.roll_offset, which are then used as new view offsets. The function can also do other things, such as call the lookat() method to temporarily set heading and pitch. See the bo105 for an example. While further minor changes are to be expected, the configuration method seems to be the way to go.
This commit is contained in:
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0529f66842
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1 changed files with 77 additions and 67 deletions
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@ -103,26 +103,26 @@ ViewManager = {
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m.roll_axis = ViewAxis.new("/sim/current-view/goal-roll-offset-deg");
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m.roll_axis = ViewAxis.new("/sim/current-view/goal-roll-offset-deg");
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# accelerations are converted to G (one G is subtraced from z-accel)
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# accelerations are converted to G (one G is subtraced from z-accel)
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m.axI = Input.new("/accelerations/pilot/x-accel-fps_sec", 0.03108095, 0, 0.58, 0);
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m.ax = Input.new("/accelerations/pilot/x-accel-fps_sec", 0.03108095, 0, 0.58, 0);
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m.ayI = Input.new("/accelerations/pilot/y-accel-fps_sec", 0.03108095, 0, 0.95);
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m.ay = Input.new("/accelerations/pilot/y-accel-fps_sec", 0.03108095, 0, 0.95);
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m.azI = Input.new("/accelerations/pilot/z-accel-fps_sec", -0.03108095, -1, 0.46);
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m.az = Input.new("/accelerations/pilot/z-accel-fps_sec", -0.03108095, -1, 0.46);
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# velocities are converted to knots
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# velocities are converted to knots
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m.vxI = Input.new("/velocities/uBody-fps", 0.5924838, 0, 0.45);
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m.vx = Input.new("/velocities/uBody-fps", 0.5924838, 0, 0.45);
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m.vyI = Input.new("/velocities/vBody-fps", 0.5924838, 0);
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m.vy = Input.new("/velocities/vBody-fps", 0.5924838, 0);
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m.vzI = Input.new("/velocities/wBody-fps", 0.5924838, 0);
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m.vz = Input.new("/velocities/wBody-fps", 0.5924838, 0);
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# turn WoW bool into smooth values ranging from 0 to 1
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# turn WoW bool into smooth values ranging from 0 to 1
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m.wowI = Input.new("/gear/gear/wow", 1, 0, 0.74);
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m.wow = Input.new("/gear/gear/wow", 1, 0, 0.74);
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m.hdg_change = aircraft.lowpass.new(0.95);
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m.hdg_change = aircraft.lowpass.new(0.95);
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m.ubody = aircraft.lowpass.new(0.95);
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m.ubody = aircraft.lowpass.new(0.95);
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m.last_heading = m.headingN.getValue();
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m.last_heading = m.headingN.getValue();
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m.size_factor = -getprop("/sim/chase-distance-m") / 25;
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m.size_factor = -getprop("/sim/chase-distance-m") / 25;
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if (props.globals.getNode("rotors", 0) != nil) {
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if (props.globals.getNode("rotors", 0) != nil) {
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m.default_helicopter();
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m.calculate = m.default_helicopter;
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} else {
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} else {
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m.default_plane();
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m.calculate = m.default_plane;
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}
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}
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m.reset();
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m.reset();
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return m;
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return m;
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@ -140,87 +140,82 @@ ViewManager = {
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me.roll_axis.add_offset();
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me.roll_axis.add_offset();
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},
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},
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apply : func {
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apply : func {
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if (me.lookat_active) {
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me.heading_axis.prop.setValue(me.lookat_heading);
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me.pitch_axis.prop.setValue(me.lookat_pitch);
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return;
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}
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me.pitch = me.pitchN.getValue();
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me.pitch = me.pitchN.getValue();
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me.roll = me.rollN.getValue();
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me.roll = me.rollN.getValue();
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me.wow = me.wowI.get();
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me.calc != nil and me.calc();
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me.calculate();
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me.calc_heading != nil and me.heading_axis.apply(me.calc_heading());
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if (!me.lookat_active) {
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me.calc_pitch != nil and me.pitch_axis.apply(me.calc_pitch());
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me.heading_axis.apply(me.heading_offset);
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me.calc_roll != nil and me.roll_axis.apply(me.calc_roll());
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me.pitch_axis.apply(me.pitch_offset);
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},
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me.roll_axis.apply(me.roll_offset);
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lookat : func(h = nil, p = nil) {
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}
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if (h == nil) {
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},
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view.resetView();
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lookat : func(heading = nil, pitch = nil) {
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me.lookat_active = 0;
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if (heading != nil and pitch != nil) {
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return;
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me.lookat_active = 1;
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me.heading_axis.apply(heading);
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me.pitch_axis.apply(pitch);
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me.roll_axis.apply(0);
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} else {
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me.lookat_active = 0;
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me.heading_axis.apply(me.heading_offset);
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me.pitch_axis.apply(me.pitch_offset);
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me.roll_axis.apply(me.roll_offset);
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}
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}
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me.lookat_heading = h;
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me.lookat_pitch = p;
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me.lookat_active = 1;
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},
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},
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};
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};
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# default calculations for a plane
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#
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ViewManager.default_plane = func {
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ViewManager.default_plane = func {
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me.calc = func {
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var wow = me.wow.get();
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# calculate steering factor
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var hdg = me.headingN.getValue();
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var hdiff = normdeg(me.last_heading - hdg);
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me.last_heading = hdg;
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me.steering = normatan(me.hdg_change.filter(hdiff)) * me.size_factor;
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me.az = me.azI.get();
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# calculate steering factor
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me.vx = me.vxI.get();
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var hdg = me.headingN.getValue();
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var hdiff = normdeg(me.last_heading - hdg);
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me.last_heading = hdg;
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var steering = normatan(me.hdg_change.filter(hdiff)) * me.size_factor;
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# calculate sideslip factor (zeroed when no forward ground speed)
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var az = me.az.get();
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var wspd = me.wind_speedN.getValue();
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var vx = me.vx.get();
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var wdir = me.headingN.getValue() - me.wind_dirN.getValue();
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var u = me.vx - wspd * cos(wdir);
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me.slip = sin(me.slipN.getValue()) * me.ubody.filter(normatan(u / 10));
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}
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me.calc_heading = func { # heading
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# calculate sideslip factor (zeroed when no forward ground speed)
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var wspd = me.wind_speedN.getValue();
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var wdir = me.headingN.getValue() - me.wind_dirN.getValue();
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var u = vx - wspd * cos(wdir);
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var slip = sin(me.slipN.getValue()) * me.ubody.filter(normatan(u / 10));
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me.heading_offset = # heading
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-15 * sin(me.roll) * cos(me.pitch) # due to roll
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-15 * sin(me.roll) * cos(me.pitch) # due to roll
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+ 40 * me.steering * me.wow # due to ground steering
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+ 40 * steering * wow # due to ground steering
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+ 10 * me.slip * (1 - me.wow) # due to sideslip (in air)
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+ 10 * slip * (1 - wow); # due to sideslip (in air)
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}
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me.calc_pitch = func { # pitch
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me.pitch_offset = # pitch
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10 * sin(me.roll) * sin(me.roll) # due to roll
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10 * sin(me.roll) * sin(me.roll) # due to roll
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+ 30 * (1 / (1 + math.exp(2 - me.az)) # due to G load
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+ 30 * (1 / (1 + math.exp(2 - az)) # due to G load
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- 0.119202922) # [move to origin; 1/(1+exp(2)) ]
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- 0.119202922); # [move to origin; 1/(1+exp(2)) ]
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}
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me.calc_roll = nil;
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me.roll_offset = 0;
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}
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}
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# default calculations for a helicopter
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#
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ViewManager.default_helicopter = func {
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ViewManager.default_helicopter = func {
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me.calc = func {
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var lowspeed = 1 - normatan(me.speedN.getValue() / 20);
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me.lowspeed = 1 - normatan(me.speedN.getValue() / 20);
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}
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me.calc_heading = func { # view heading due to
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me.heading_offset = # view heading due to
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-50 * npow(sin(me.roll) * cos(me.pitch), 2) # roll
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-50 * npow(sin(me.roll) * cos(me.pitch), 2); # roll
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}
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me.calc_pitch = func { # view pitch due to
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me.pitch_offset = # view pitch due to
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(me.pitch < 0 ? -35 : -40) * sin(me.pitch) * me.lowspeed # pitch
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(me.pitch < 0 ? -35 : -40) * sin(me.pitch) * lowspeed # pitch
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+ 15 * sin(me.roll) * sin(me.roll) # roll
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+ 15 * sin(me.roll) * sin(me.roll); # roll
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}
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me.calc_roll = func { # view roll due to
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me.roll_offset = # view roll due to
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-15 * sin(me.roll) * cos(me.pitch) * me.lowspeed # roll
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-15 * sin(me.roll) * cos(me.pitch) * lowspeed; # roll
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}
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}
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}
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@ -239,6 +234,18 @@ main_loop = func(id) {
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}
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}
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var calc = nil;
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register = func(f) {
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calc = f;
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}
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reset = func {
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view_manager.reset();
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}
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lookat = func(heading = nil, pitch = nil) {
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view_manager.lookat(heading, pitch);
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}
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var original_resetView = nil;
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var original_resetView = nil;
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var panel_visibilityN = nil;
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var panel_visibilityN = nil;
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@ -256,7 +263,7 @@ var L = []; # vector of listener ids; allows to remove all listeners (= useless
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# Initialization.
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# Initialization.
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#
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#
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setlistener("/sim/signals/fdm-initialized", func {
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settimer(func {
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# disable menu entry and return for inappropriate FDMs (see Main/fg_init.cxx)
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# disable menu entry and return for inappropriate FDMs (see Main/fg_init.cxx)
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var fdms = {
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var fdms = {
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acms:0, ada:0, balloon:0, external:0,
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acms:0, ada:0, balloon:0, external:0,
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@ -294,6 +301,9 @@ setlistener("/sim/signals/fdm-initialized", func {
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}, 1));
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}, 1));
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view_manager = ViewManager.new();
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view_manager = ViewManager.new();
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if (calc != nil) {
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view_manager.calculate = calc;
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}
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original_resetView = view.resetView;
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original_resetView = view.resetView;
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view.resetView = func {
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view.resetView = func {
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@ -315,6 +325,6 @@ setlistener("/sim/signals/fdm-initialized", func {
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append(L, setlistener("/sim/signals/reinit", func {
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append(L, setlistener("/sim/signals/reinit", func {
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view_manager.reset();
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view_manager.reset();
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}, 0));
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}, 0));
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});
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}, 0);
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