Commit 5f0066c resulted in an incorrect angle calculation. At certain view/sun
angles "hor_rotation" and "rf1" would skip from the minimum to the maximum
value).
Also, an offset angle of 90 degrees (PI/2) is added, which seems to align
the sky effect with the sun position. Calculation is probably still wrong,
but seems less wrong than before - and the flickering is gone...
- initialize uninitialized properties
- use prefix instead of postfix increments
- reduce visibility of variables
- use empty() instead of size() == 0 for vector and string
- pass string by reference, not by value
Avoid using the now deprecated readObjectModelTemplate() method
in HLAFederate. Make more use of the available general
initialization functions in HLAFederate.
Give details whether includes or libraries are missing,
or if (and how) the version mismatches.
Also require an exact simgear/flightgear version match.
This property is true if the active frequency is tuned to a
paired LOC/GS frequency in the range 108.00 - 111.95 with a
odd 100kHz digit (108.10, 108.15, 108.30, 108.35 ...)
It only indicates, that this _is_ a LOC/GS frequency,
it does _not_ provide any indication if a LOC/GS station is
actually being received.
- Add update-interval-secs to the entire autopilot
- cache min/max values in InputValue
- a little more relaxed "equals zero" checking in the NoiseSpikeFilter
Some things about fltk seem changed, which broke fgadmin:
fl_filename_list could return negative number instead of 0.
fl_filename_list now has a "/" appended to every reported directory name.
free( list ) now caused a segfault - use fltk's method to free memory.
fgadmin should now work with new and old Fltk.
- add new <update-interval-secs> for autopilot components.
This does what it says.
- add new method to PeriodicalValue to normalize symmetric around zero
- move the DigitalFilterImplementation out of the header file
- refactor NoiseSpikeFilter: spare some cpu-cycles and respect periodical
output
The property /fdm/jsbsim/propulsion/engine/prop-induced-velocity_fps
gives wrong answers, and can become NaN under certain conditions. When thrust is
negative and forward velocity is small we can take the square root of a negative
number. This could occur, for example, when using reverse thrusters on landing.
The value comes out much too high when alpha is near 180, such as taxing with a
tail wind.
