- tidies up the update-time-step handling (making it a simple "dt");
- makes the altimeter get a proper pressure, and the (unused) vacuum
calculation get a proper RPM (*);
- replaces property name look-ups with static pointers to property nodes.
Notes from DPM:
- the static pointers are a very bad idea, but they're only temporary;
I plan to make FGSteam into a proper subsystem soon, and then they
can be member variables
- I fixed the patch to get the current static pressure from the
/environment/pressure-inhg property, so that the altimeter interacts
properly with FGEnvironment
The present sets of bindings result in the throttle being "squared"
about its centre, which is silly. This is because the "squared"
parameter is not set by the throttle binding, but the default is
"true". We discussed this before and I think there was general
agreement that the default should be "false" on the basis of
generality.
situations for every kind of airplane. But at the moment we have nothing
implimented and this will cover the simpler cases until someone has a
chance to impliment a fuller solution.
GL/gl.h can't be included at the first position in windows. It requires
the inclusion of windows.h that must be included in other fgfs header
file. I only move down #include <GL/gl.h>
This patch eliminates about 10 of valgrind's "Use of uninitialised
value of size ..." messages. They are all caused by approachlist building
incomplete FGApproach class instances and then copying them into the
approchlist container, hence copying data garbage.
I know, I couldn't win a beauty contest with this patch, but the
alternative approach -- letting operator<< always leave complete
entries -- didn't look any better. And I do only add those seemingly
useless initialization where the values would be used uninitialized
else. The constructors are only run during setup and won't slow fgfs
down at runtime.
Make locally-used strings local instead of global. (The safety and
cleanliness benefit outweights the slight performance hit. If
performance is an issue, the way these strings are used should be
optimised.) Use existing defined constant instead of a literal
number.
+ The panel(s) are now an first-class SSG node inside the aircraft
scene graph. There's a little code added to model.cxx to handle the
parsing, but most of the changes are inside the new FGPanelNode
class (Model/panelnode.[ch]xx).
+ The old FGPanel source changed a lot, but mostly cosmetically. The
virtual-cockpit code moved out into FGPanelNode, and the core
rendering has been abstracted into a draw() method that doesn't try
to set any OpenGL state. I also replaced the old inter-layer offset
code with glPolygonOffset, as calculating the right Z values is hard
across the funky modelview matrix I need to use. The older virtual
panel code got away with it by disabling depth test, thus the "panel
draws on top of yoke" bug. PolygonOffset is really the appropriate
solution for this sort of task anyway.
+ The /sim/virtual-cockpit property is no more. The 2D panels are
still specified in the -set.xml file, but 3D panels are part of the
model file.
+ You can have as many 3D panels as you like.
Problems:
+ The mouse support isn't ready yet, so the 3D panels still aren't
interactive. Soon to come.
+ Being part of the same scene graph as the model, the 3D panels now
"jitter" in exactly the same way. While this makes the jitter of
the attitude gyro less noticeable, it's still *very* noticeable and
annoying. I looked hard for this, and am at this point convinced
that the problem is with the two orientation computations. We have
one in FGLocation that is used by the model code, and one in
FGViewer that is used at the top of the scene graph. My suspicion
is that they don't agree exactly, so the final orientation matrix is
the right answer plus the difference. I did rule out the FDMs
though. None of them show more than about 0.0001 degree of
orientation change between frames for a stopped aircraft. That's
within an order of magnitude of what you'd expect for the
orientation change due to the rotation of the earth (which we don't
model -- I cite it only as evidence of how small this is); far, far
less than one pixel on the screen.
[and later]
OK, this is fixed by the attached panel.cxx file. What's happened is
that the winding order for the text layer's polygons is wrong, so I
reverse it before drawing. That's largely a hatchet job to make
things work for now, though. We should figure out why the winding
order is wrong for only text layers and fix it. I checked the plib
sources -- they're definitely doing things CCW, as is all the rest of
the panel code.
Odd. I'm also not sure why the 2D panel doesn't care (it works in
both winding orders). But this will allow you to check in working
code, anyway. There's a big comment to this effect in there.
instrument. This needs to move somewhere permanent.
Also, remove a bogus fuel consumption setting that (1) was off by a factor
of 3600 (hours, not seconds) and (2) collided with identical code in FGFDM.
the amount of drag that the produced lift *would* have produced given an
unflapped air surface. A nifty trick involving the assumption that AoA is
small works for this, and produces plausible results in the high AoA case
as well.
Also, trim for approach using the elevator-trim control, not elevator.
Just cosmetic for current planes, but future ones might have differing
implementations of trim.
This is the small code fix which is needed for the new options.xml file.
It is needed because otherwise the "--prop:name=value" is showed
incorrectly.
There is another problem though, when compiling with --without-logging
the help message isn't displayed at all! We *must* change that somehow.
Curt: good point, the SG_LOG()'s have been switched to cout's ...
(and not the throttle setting), but the recalculation left in a degeneracy
when the target/throttle setting was exactly zero. Zero times a big number
is still zero. Fixed to use real math, not theoretical math.
- More progress with proper radio freq tuning and proper interpreting of the
hardware values.
- Filter ignition and flap switch values since the hardware implimentation has
a dead zone where the value can go to zero in the middle of a change in
switch position.
I've updated the FIXME in the code, and fixed a typo (descr instead of
description), but the SG_LOG() functions doesn't produce any output for
me. Could you confirm it's still working for you?
Curt Olson:
I did a bit of further tweaking and it all looks good now. The tricky thing
is that SG_LOG() always appends an endl at the end of every message.
This is an enhanced version of the options patch.
It's more robust now, and gives some helpful information if something
goes wrong. Also the naming in the options.xml file has changed to the
syntax David suggested.
Since no one objected to the patch I think it is safe to included it.
class, FGModelPlacement, while FG3DModel retains control of animation.
This way, we can have a single, top-level placement, but multiple
layers of nested models underneath. To include a nested model, use
something like this in the XML wrapper:
<model>
<path>Models/Stuff/my-component.xml</path>
<offsets>
<roll-offset-deg>45</roll-offset-deg>
</offsets>
</model>
contain colon-separated ranges. For examples, winds from 180 degrees
10 knots gusting 15 knots would be
--wind=180@10:15
Winds variable from 180-220 degrees 5 knots would be
--wind=180:220@5
FGEnvironment does not yet support variable-direction winds, so
nothing will yet happen in the second case.
Modifications to support querying navaid database by station ID (not just
frequency.) Some corresponding changes to testnavs.cxx to test new
functionality.
This is a small patch that makes the autopilot work much better with big heavy
airliners as well as the small Cessnas. Of course this doesn't address the
way autopilots should be modeled.
But by making a couple changes the "George" is now capable of landing either a
C172 or a 747 very close to the center line of the runway with a moderate
cross breeze (15-20kt).
The changes:
- Added turn configurability so that things like Max Aileron and Roll can be
configured per aircraft.
- Enhanced localizer routine (NAV mode) to begin lining up the aircraft as soon
as the cone is entered. The former model is adopted for the last 5km of the
approach in order to ensure greater precision (makes a very slight difference).
[float cast added by David Megginson to keep G++ 3.0 happy]
This is a small patch that makes the autopilot work much better with big heavy
airliners as well as the small Cessnas. Of course this doesn't address the
way autopilots should be modeled.
But by making a couple changes the "George" is now capable of landing either a
C172 or a 747 very close to the center line of the runway with a moderate
cross breeze (15-20kt).
The changes:
- Added turn configurability so that things like Max Aileron and Roll can be
configured per aircraft.
- Enhanced localizer routine (NAV mode) to begin lining up the aircraft as soon
as the cone is entered. The former model is adopted for the last 5km of the
approach in order to ensure greater precision (makes a very slight difference).
[float cast added by David Megginson to keep G++ 3.0 happy]
1. Typo where /environment/density-inhg instead of
/environment/density-slugft3 was flagged as archivable.
2. Density should no longer be archivable anyway, since it is
calculated internally and not directly settable by the user.
temperature, and dewpoint. The /environment/density-sea-level-slugft3
property has been removed, and the /environment/density-slugft3
property is read-only.
Fetch all pending remote fdm network packets so there is not chance of
getting behind.
Add support for driving control panel lights.
Working on better modeling KX 155 tuning behavior.
won't apply the right gross weight due to fuel differences.
When solving for zero force, do so in the global frame, not the
aircraft's. In principle, this shouldn't matter (zero is zero in all
frames), but in practice this should help to avoid oscillations.
Calculating lift as force perpendicular to the ground (and not the
wing plane) is clearly the Right Thing, anyway.
Also added support for a /yasim/gross-weight-lbs property, which
should be generically useful.
when the lift/drag are really solid. And defer the approach trim until
the all four of the other variables are perfect. I believe this should
fix the solution failures under gcc 2.95.2.
implicitly in PropEngine by disallowing negative torques, but that was
removed at some point. We really need the explosion protection here
at the source.
This patch adds "elapsed time" support to the sound code.
It is now possible to define <internal>dt_play</internal> or
<internal>dt_stop</internal> instead of a propery in the <volume> and
<pitch> sections of the configuration file.
