You are right with your second point about the two airfields, but I
think we should let the pilot figure this out. I guess I would have to
agree that the time spent circling shouldn't be a factor. AFAIK no
other software does it that way... As I mentioned earlier, we could
make it configurable but I don't think that's really useful.

Turbo

2011/11/21 John Wharington <jwharing...@gmail.com>:
> We will have to agree to disagree on that.
> Arrival altitude should indeed consider circling, and you should set a
> reasonable MC value, if you are able to climb.  If you don't expect to
> be able to climb, then set MC=0.
>
> If conditions are such that climbing in weak lift makes an upwind
> landing point effectively unreachable, this should be shown.  If
> downwind drift due to circling was not taken into account, then
> two airfields just beyond pure glide range would look similarly
> attractive even though in actuality, the downwind one will be much
> more reachable at a low climb rate.
>
> On Tue, Nov 22, 2011 at 3:09 AM, Ramy Yanetz <ryan...@yahoo.com> wrote:
>> Arrival altitude should NEVER consider circling! I never heard of such 
>> theory. Arrival altitude should only consider polar, degradation, wind and 
>> MC, although it would be fine without considering MC at all. But trying to 
>> guess your climb and your drift while climbing is completely wrong. We are 
>> not trying to predict the future, we are trying to tell the pilot if he can 
>> safely reach an airport or how much he needs to climb.
>>
>> Ramy
>>
>> On Nov 21, 2011, at 5:43 PM, Tobias Bieniek <tobias.bien...@gmx.de> wrote:
>>
>>> John, I think this is inconsistent behaviour... either if you can't
>>> climb you shouldn't see the pure glide value, or if you have a MC
>>> above 0 you shouldn't consider the wind effect while circling. Maybe
>>> for internal calculations we should supply both values and let the
>>> user decide what he wants to see.
>>>
>>> Turbo
>>>
>>>
>>>
>>> 2011/11/21 John Wharington <jwharing...@gmail.com>:
>>>> This is not a bug.
>>>>
>>>> At MC=0, you cannot climb, so the value reported (-500 feet) indicates
>>>> you magically need to gain 500 feet in order to glide at MC=0.
>>>>
>>>> At MC=0.5, you are telling the computer you can climb, and with that
>>>> headwind and a slow climb rate (0.5), you need to climb a lot more.
>>>> In this case, the 500 feet isnt obtained magically, and so the height
>>>> required takes the downwind drift from circling into account.
>>>>
>>>> On Tue, Nov 22, 2011 at 1:34 AM, Ramy Yanetz <ryan...@yahoo.com> wrote:
>>>>> Arrival altitude was at MC =0 was something like -500 feet (500 feet 
>>>>> below glide) which was correct. However, With MC=0.5 it was -6000 feet!!! 
>>>>> This is obviously a bug since the slight increase in MC will never result 
>>>>> in 5000 feet loss.
>>>>
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>

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