8:: AWOS is available at AWOS locations. (Previously only ATIS was
implemented.)
9:: ATIS phraseology now more nearly conforms to international
standard METAR pattern, and therefore to usual FAA practice.(*)
Items marked with a (*) are fully implemented in the /text/ of the
ATIS message, but the voiced version of the message is degraded by
limitations of the FGFS built-in text-to-speech system.
10:: ATIS now reports sky condition.(*)
11:: ATIS now reports multiple layers of clouds, not just the lowest
layer.(*)
12:: ATIS now takes field elevation into account when calculating
sky condition and ceiling.
13:: ATIS now reports dewpoint.(*)
14:: ATIS now can handle negative quantities (temperature and dewpoint).(*)
15:: ATIS can now report report fractional-mile visibility.(*)
16:: ATIS now uses magnetic (not true) wind directions, as it should.
17:: ATIS generates correct runway number and suffix (nine right,
one one left).
18:: ATIS can be received on nav frequencies, not just comm.
19:: Nothing bad happens if the same ATIS is tuned up on more than
one receiver.
20:: ATIS can be updated at times other than at the top of the hour.
21:: ATIS listens for an "attention" signal, and responds to changes
in the weather by issuing a new ATIS message (somewhat like a
"special observation").
22:: ATIS volume now responds to radio volume setting.
23:: Area-related services (i.e. approach radar) are handled
more-nearly consistently with radio-frequency related services.
24:: ATIS sequence-letter generation has been fixed.
25:: ATIS messages are now in the property tree, so they can be read
e.g. via the http interface.
John Denker's atmosphere changes. Original commit message:
Two-parameter physics-based model of atmosphere up to 262,467 ft i.e.
the top of the mesosphere. Correctly exhibits the HALT phenomenon.
- false LOC courses and GS lobes
- LOC sensitivity based on runway dimensions
- GS cutoff based on range
- More accurate GS deviation computation, making final approach more stable
Conflicts:
src/Environment/environment.cxx
src/Environment/environment.hxx
John Denker's atmosphere changes. Original commit message:
Two-parameter physics-based model of atmosphere up to 262,467 ft i.e.
the top of the mesosphere. Correctly exhibits the HALT phenomenon.
FG crashes at exit at very high likelihood.
The cause of the crash is that some subsystems (input and gui) call get_subsystems() at their destructor.
This is very dangerous since SGSubSystemMgr::get_subsystem() can refer to already deleted subsystems.
Fixed: wrong event name for abs-hat0-y
Modified: let AxisElement to generate normalized input (-1.0 to 1.0).
This can be temporal and can be removed when AxisEvent normalizes its value.
Modified: clean up code
Added: some comments so other Mac developers can see what's going on
Additionally to the original fix (problem with the Tec2b matrix initialization) I have modified the code for the "STRUCTURE" contacts in order not to generate NaNs when the z direction of the body frame is normal to the ground normal. Now there should no longer be any NaN generated by the landing gear code.
- Make sure to initialize the groundnetwork after succesful loading.
- Ensure that the AI groundnetwork code proximity detection code used the
correct values for bearing. (Note that detecting the proximity of the
user aircraft appears still to be broken. I'll look into that later).
