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Author SHA1 Message Date
curt
ec50bcfb5a Roy Ovesen:
I've added some features to the PID controller:

Ability to set desired sampling interval in seconds. Use <Ts> under <config>
to set the desired sampling interval of the PID controller.

Example:
<config>
     <Ts>0.1</Ts>        <!-- desired sampling interval -->
     <Kp>-0.05</Kp>        <!-- proportional gain -->
     <beta>1.0</beta>    <!-- input value weighing factor -->
     ...
     ...
</config>

Ts defaults to 0.0, so if you don't set it it samples at the highest possible
frequency.


Add an offset to the input variables (input and reference).
Example:
    <reference>
      <prop>/controls/flight/elevator</prop>
      <scale>-1.5</scale>
      <offset>1.0</offset>
    </reference>

Note that <scale> has higher precedence than <offset>, regardless of the order
that they appear in the config file.
2005-02-01 21:00:24 +00:00
ehofman
4d8da078a4 Roy Vegard Ovesen:
I guess it is much more efficient to compare integers than comparing long strings like "double-exponential" every frame.
2005-01-20 09:55:47 +00:00
curt
c6f0d87a26 A few more radios -> instrumentation name changes thanks to Melchior for
catching these.
2004-12-04 21:06:57 +00:00
curt
d05121ef46 Fix my mailing address by replacing it with my web page. 2004-11-19 22:10:41 +00:00
ehofman
fa7f2468c2 Roy Vegard Ovesen:
I've added some digital filters to the autopilot. They are all low-pass
filters that filter away high frequency signals/noise. There are 4 different
filters:

1. Exponential - The algorithm is essentially the same as the one used in the
   fgGetLowPass() function.

2. Double exponential - Two exponential filters in series. This filter has a
   "steeper" frequency response curve. It filters "better" than the single
   exponential.

3. Moving average - Averages a number of inputs.

4. Noise spike - limits the amount that the output value can change from one
   sample to the next.

Filters 1 and 2 are characterised by it's filter-time in seconds. For filter 3
you have to set the number of input samples to average over. For filter 4 you
set the maximum allowed rate of change as [1/s]. Since the sampling interval
(dt) isn't constant we have to calculate the maximum allowed change for every
update.

Example of a double exponential filter with filter time 0.1 seconds, that is
1/0.1 = 10 Hz.

  <filter>
    <name>pressure-rate-filter</name>
    <debug>true</debug>
    <type>double-exponential</type>
    <input>/autopilot/internal/pressure-rate</input>
    <output>/autopilot/internal/filtered-pressure-rate</output>
    <filter-time>0.1</filter-time>
  </filter>

This would go in the autopilot configuration file.

I've also removed the filtering of the "pressure-rate" helper value, use the
new filters if you want to filter it!  ;-)
2004-10-14 09:19:44 +00:00
curt
088a7a83b4 Add a pressure rate helper function for Roy's KAP140 autopilot model. 2004-04-12 19:17:47 +00:00
curt
2acdd02879 Clean up various compiler warnings that have crept into the code. This
by no means get's them all, but it's a start.
2004-04-01 15:27:53 +00:00
curt
0857271582 Jim Wilson:
This patch adds the ability to do a simple scaling of input without having to
add hardcoded helpers.  Example:

    <reference>
      <prop>/autopilot/settings/vertical-speed-fpm</prop>
      <scale>0.01667</scale>
    </reference>
2004-03-21 21:05:06 +00:00
curt
2845a75753 Jim Wilson:
Add FGPredictor class to xmlauto.  Add support for horizontal navigation based
on flight track as opposed to heading.  Add crosstrack-error support to nav.
Simplify error adjust calculation for horizontal nav (better interception).
Fixed potential divide by zero that was producing nan issues in the xmlauto
code.
2004-03-19 03:23:28 +00:00
curt
ea39c09192 Make sure delta_u_n and u_n are always explicitely initialized. 2004-03-15 19:15:40 +00:00
curt
a5f9927727 Roy Vegard Ovesen:
I've done some changes to xmlauto.cxx.

Only calculate the derivate filtering if derivate time Td is greater than
zero. This means that one can set Td=0.0 in the xml file to completely remove
the derivate action. (Setting Td to zero in the current version would lead to
a division by zero and crash.)

Setting the integrator time Ti to zero doesn't make sense, right! I've
modified so that setting Ti to zero results in the integral action being
completely removed.
2004-03-15 19:09:44 +00:00
curt
71c83c4de7 Initialize autopilot output to start at current manual control position
to [hopefully] make autopilot activation less "dramatic."
2004-02-12 22:35:29 +00:00
curt
bffca78da4 Add my old ultra-simplistic PI controller. The fancy PID controller doesn't
seem to be fully deterministic in P-only mode.  This old simple controller
does what I expect, so it's good for calulating stage #1's of multi-stage
controllers.
2004-02-05 17:11:47 +00:00
curt
266534259d Add vertical speed fpm conversion since the fdm provides this value in
fps.
2004-02-04 20:16:30 +00:00
curt
8191e743f0 Cleaned up some left over stuff. Working towards infrastructure to support
adding additional PID type algorithms to the code.
Add support for calculating heading bug error relative to magnetic heading
for slaved DG's.
2004-02-04 17:10:32 +00:00
curt
c4bca03ec2 autopilot reinit() now reloads config file. 2004-02-03 20:17:57 +00:00
curt
348d3e26ce Comment out some unused references and left over debugging output. 2004-02-03 19:34:23 +00:00
curt
da5ea10d5d Curt Olson:
Autopilot overhaul.
2004-01-31 19:47:45 +00:00