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Coupled approach?



 
 
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  #1  
Old September 26th 04, 01:27 PM
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My two cents worth: any autopilot that acts in that manner is probably
best not used for "coupled" approaches. I put "coupled" in quotes
because a truely coupled approach would be independent of the heading
bug once the localizer has been captured.

The kludged-up situation you describe could be hazardous during
demanding circumstances.

Roy Smith wrote:

In article ,
"Jeremy Lew" wrote:


Don't know anything about that A/P, but I was under the general impression
that if an A/P is in APR or NAV mode, it is following the CDI needle (or
possibly the GPS?). The heading bug is used for HDG mode.



Well, the manual says:

"In systems equipped with a DG, during an instrument approach, the
heading bug must be set to match course for the segment of the approach
being flown when using the NAV, APR, or REV modes. course pointer."

Unfortunately, the manual is big on rote descriptions of which buttons
to push when, and says damn near nothing about how the thing actually
works inside. I'm left with guessing at its operating logic based on
observed behavior and some theoretical knowledge of control systems.

Clearly, setting the heading bug 10 degrees off the desired course was a
mistake, but the manual doesn't even begin to talk about the best way to
correct the mistake. Just resetting the bug to the right setting
resulted in course oscillations. What I'm trying to figure out is what
might have been a better course of action.


  #3  
Old September 27th 04, 03:55 PM
Michael
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wrote
My two cents worth: any autopilot that acts in that manner is probably
best not used for "coupled" approaches.


I concur. But then I'm not a fan of doing coupled approaches with
old-technology autopilots anyway.

I put "coupled" in quotes
because a truely coupled approach would be independent of the heading
bug once the localizer has been captured.


Do you fly an approach without reference to heading once the localizer
is captured? Of course not - you fly a heading, and use the CDI as a
correction on the heading. So do most Century autopilots. There is
nothing wrong with using heading information to stabilize the
approach. The problem is with the way the unit does it.

Century 2000 sounds all nice and modern, but really it's the same old
analog control loop design going all the way back to the Century II
with a digital false face hung on it. Here's how it really works:

At its core, the device is a wing leveler, and a crude one at that.
It runs a roll servo to attempt to keep the bank angle at some
setpoint. That set point can be zero bank, it can be some bank angle
dialed in by a roll knob, or it can come from the heading gyro. In
that case, the set point is a bank angle proportional to the deviation
between actual and bugged heading, with a limit (usually 25 degrees of
bank). When a nav coupler is used, the nav deviation is used to add
an offest to the bug. What I mean by this is, let's say in LOC mode,
one dot is worth five degrees. If the loc needle is a dot right, then
the nav converter will make the autopilot think that the bug is five
degrees to the right of where you set it. In reality, it's usually
not linear - past some point (say 3/4 scale) it will start making each
additional increment worth a lot more degrees, so that it can track a
course somewhat even if the user set the bug totally wrong. So really
we have another control loop, and a non-linear one at that.

Now, obviously with this kind of scheme, you never actually eliminate
offset unless you set the heading bug to the correct heading (not
course) to fly. That's why the approach was being flown two dots out.
This is normal behavior for the Century system.

The problem is that when the heading bug was reset, the system went
into oscillatory behavior.

Realize, though, that this is a system with three nested control loops
- a tight inner loop doing wing leveling, a more damped loop modifying
the bank angle setpoint on the inner loop based on heading deviation
to accomplish heading hold, and a third loop modifying the heading
setpoint on the middle loop based on course deviation to accomplish
course tracking.

Now realize that ultimately, that inner loop is deflecting ailerons -
and air loads on ailerons at any given bank angle depend quite a lot
on airspeed, not to mention control system friction (which can vary
with rigging and ambient temperature). The system is expected to work
over a range of airspeeds and temperatures for a given make and model,
and with only minor tweaks it is the same system for many makes and
models.

Note that turbulence will affect bank angle - adding noise into the
system.

The rate of heading change as a function of bank angle changes with
airspeed. Once again the system is expected to work over a range of
airspeeds.

The rate of angular course deviation as a function of heading change
depends on distance from the navaid and groundspeed. The system is
expected to function over a range of distances and groundspeeds.

It's pretty damn tough to do a triple nested control loop with
reasonably fast response across a variety of conditions and not have
oscillatory behavior somewhere. There are lots of adjustments to be
made. Then rigging changes over the years, things maybe don't get
lubed quite so well as they sould, electronic components drift out of
tolerance due to temperature extremes as the plane sits out in the sun
and heats up to 130 or chills in the winter to -20.

So the bottom line is what you saw is not so unusual, and the correct
solution (assuming there is one that does not involve hand flying)
will depend on what has drifted out of tolerance. Changing heading in
steps may be the way - usually the smaller the setpoint change the
lower the chance of oscillatory behavior. But the reality is that you
have an autopilot that, while still usable for lots of things, is
probably not quite exactly right, and probably should not be used for
actual coupled approaches. Which is pretty much the norm for older GA
autopilots.

Michael
  #5  
Old September 28th 04, 07:52 PM
James M. Knox
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wrote in
link.net:

I make reference to the heading, but once coupled I have no autopilot
input to modify or adjust heading in any manner, so I certainly do not
fly heading while in NAV, APPROACH, or AUTOLAND modes. If I am hand
flying using the flight director while in NAV or APPROACH modes then,
indeed, I am using heading to track the course (course and vertical
path in case of ILS). But, the autopilot completely takes over
steering of heading when its doing the task, as its alway been with
any autopilot I've used since 1960 or so.


But not so with most of the Century autopilots out there, including ones
installed as late as 1980's). While the newer ones do as you describe,
all the older ones utilize a combination of data from the AI, DG, and
NAV input.

The AI provides the "wing leveler" primary input, while the DG and NAV
signals are summed to provide a heading. Amazingly effective, for such
a trivial analog approach, it will (if carefully adjusted) intercept and
track a NAV signal. However, in a strong crosswind, it will do so "off"
the actual courseline (parallel to it). The Century manual states that
"if this bothers you" you should simply adjust the heading bug on the DG
to an amount "offset" the other way.

The two annoying features of this system a
1. Every time the desired course changes, you have to adjust the heading
bug on the DG accordingly.

2. Like all such systems, there is no turn anticipation. So it is
always a compromise on each new acquisition between undershoot and
overshoot. These systems have a sensitivity adjustment that sets this.
Problem is: a) too little, and it will fly S-turns about the desired
course line, and b) too much, and it will wing rock itself until you
toss your cookies. Getting it set "just right" is an inflight specific
adjustment unique to each individual autopilot unit and N# combo.

jmk
  #6  
Old September 28th 04, 11:44 PM
Roy Smith
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"James M. Knox" wrote:
The AI provides the "wing leveler" primary input, while the DG and NAV
signals are summed to provide a heading. Amazingly effective, for such
a trivial analog approach, it will (if carefully adjusted) intercept and
track a NAV signal. However, in a strong crosswind, it will do so "off"
the actual courseline (parallel to it).


Not quite parallel, but rather with a constant CDI offset, which for VOR
and LOC signals means a constant angular displacement.

2. Like all such systems, there is no turn anticipation.


I've never let the Century AP's fly anything but the most shallow turns.
I generally disengage the AP approaching the fix, hand-fly the turn,
then give the stick back to Otto for the next straight segment. In
fact, most of the time I just leave it in heading mode.

a) too little, and it will fly S-turns about the desired
course line, and b) too much, and it will wing rock itself until you
toss your cookies. Getting it set "just right" is an inflight specific
adjustment unique to each individual autopilot unit and N# combo.


I once flew a plane that had a *way* underdamped roll-rate. If you
reset the heading bug, it would slam you into a turn, hold that until it
was right up to the desired heading, then slam the wings back level.
IIRC, it didn't use excessive bank angles, just excessive roll rates in
and out of the turns. Not fun.
  #7  
Old September 29th 04, 02:20 PM
James M. Knox
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Roy Smith wrote in
:

"James M. Knox" wrote:
The AI provides the "wing leveler" primary input, while the DG and
NAV signals are summed to provide a heading. Amazingly effective,
for such a trivial analog approach, it will (if carefully adjusted)
intercept and track a NAV signal. However, in a strong crosswind, it
will do so "off" the actual courseline (parallel to it).


Not quite parallel, but rather with a constant CDI offset, which for
VOR and LOC signals means a constant angular displacement.


Good point... It's a constant voltage offset. I beleive one of the Century
(or old Mitchell) manuals actually uses the word parallel, but you are
right - it's a constant degree offset, only parallel for following
something like a GPS courseline.
  #8  
Old September 29th 04, 09:46 PM
PaulaJay1
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In article , Roy Smith
writes:

2. Like all such systems, there is no turn anticipation.

I've never let the Century AP's fly anything but the most shallow turns.
I generally disengage the AP approaching the fix, hand-fly the turn,
then give the stick back to Otto for the next straight segment. In
fact, most of the time I just leave it in heading mode.


Not so. My Garmin 430 when coupled to the Century will anticipate, tho with
the Archer speed,that is not much. I generally let the autopilot do the turn.
At the turn I turn the heading but to the new course and let the 430 trim it
out. If the heading change is large, I sometimes do this in two steps of half
value each.

Chuck
 




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