> -----Original Message-----
> From: [EMAIL PROTECTED] 
> [mailto:[EMAIL PROTECTED] On 
> Behalf Of Jon S. Berndt
> Sent: Saturday, July 21, 2007 2:49 PM
> To: 'FlightGear developers discussions'
> Subject: Re: [Flightgear-devel] Epsilon,alpha_tail and 
> independent tail contributions
> 
> > > We might actually be able to effectively do that, since we could 
> > > have multiple tables defined that create multipliers that 
> could be 
> > > used later.
> > >
> > > Jon
> > 
> > Well, that was going to be my initial approach, but it's a 
> real pain 
> > to remove one dimension like that out of a 4-D table to make it two 
> > 3-D tables (if I remember how that works). I haven't looked at your 
> > LFI implementation, but one that I did years ago I think used 
> > recursion, and therefore it was possible to have 'inifinty' 
> number of 
> > dimension.. Or maybe I was just working on that and never going it 
> > working. I don't know. I've spelt since then.
> > 
> > Bill
> 
> In my mind, the problem is not so much the 
> programmatic/algorithmic aspect, but how do you arrange the 
> data in our XML format in files? I've got a few ideas, but it 
> seems like it could be convoluted.
> 
> Jon
> 
> 

This is how I do 3-D data in my free-format method. Another dimension might
just be 2 entries on the "0.0" and "5000.0" lines, and there would have to
be another 2 tables, if the 4th dimension only has two values.


CP_ALTITUDE_CORRECTION_TABLE_TRAINING
   NON_DIMENSIONAL_TRUE_AIRSPEED
   SS_THRUST_COEFFICIENT
   DENSITY_ALTITUDE

   0.0

         6.377530E-03  6.799520E-03  7.671665E-03  8.155430E-03
8.714625E-03

  0.000   0.0           0.0           0.0           0.0           0.0

  0.075  -7.08702E-06  -7.46443E-06  -3.33640E-06   0.0           0.0

  0.095  -3.13841E-06  -2.70910E-06  -6.89935E-07   0.0           0.0

  0.115   9.80799E-09   2.24440E-06   3.75856E-06   0.0           0.0

  0.135   1.64757E-06   5.51617E-06   6.02906E-06   0.0           0.0

  0.155   3.16493E-06   8.90633E-06   9.08185E-06   0.0           0.0

  0.175   4.73170E-06   1.27943E-05   1.29269E-05   0.0           0.0

  0.195   6.08803E-06   1.72407E-05   1.61440E-05   0.0           0.0

  0.215   7.20410E-06   1.86653E-05   1.64733E-05   0.0           0.0

  0.235   9.13959E-06   2.25281E-05   1.90848E-05   0.0           0.0

  0.255   1.11248E-05   2.56991E-05   2.07885E-05   0.0           0.0

  0.275   1.48693E-05   3.54481E-05   2.81742E-05   0.0           0.0

  0.295   1.96035E-05   4.86056E-05   3.89821E-05   0.0           0.0

  0.315   2.43772E-05   5.99209E-05   4.68421E-05   0.0           0.0

  0.335   2.60403E-05   5.76844E-05   4.35042E-05   0.0           0.0

  0.355   3.45229E-05   6.20062E-05   4.31986E-05   0.0           0.0


   5000.0

         6.377530E-03  6.799520E-03  7.671665E-03  8.155430E-03
8.714625E-03

  0.000   0.0           0.0           0.0           0.0           0.0

  0.075  -5.82699E-06  -7.74447E-06  -3.98641E-06  -4.12238E-06
-2.16311E-06
  0.095  -2.94845E-06  -4.71913E-06  -2.63005E-06  -3.49648E-06
-2.35165E-06
  0.115  -1.14023E-06  -1.42562E-06   2.58558E-07   5.97211E-08
1.97976E-06
  0.135  -8.32457E-07   1.66066E-07   1.02905E-06   1.69658E-06
4.06150E-06
  0.155  -6.55098E-07   1.42632E-06   1.91189E-06   3.04350E-06
5.77344E-06
  0.175  -1.36832E-06   2.06431E-06   2.86690E-06   5.00068E-06
9.04538E-06
  0.195  -2.87194E-06   2.66073E-06   2.91396E-06   6.18843E-06
1.22274E-05
  0.215  -1.00594E-06   3.82526E-06   3.67334E-06   6.54650E-06
1.32896E-05
  0.235  -5.70348E-07   4.86814E-06   4.36482E-06   7.76484E-06
1.46019E-05
  0.255   9.14792E-07   5.92906E-06   4.92844E-06   9.11357E-06
1.53244E-05
  0.275  -9.10659E-07   8.20810E-06   6.30418E-06   1.05824E-05
1.77469E-05
  0.295  -4.84660E-06   9.83535E-06   7.65215E-06   1.42617E-05
2.20197E-05
  0.315  -5.64283E-06   1.19309E-05   8.17212E-06   1.69514E-05
2.69024E-05
  0.335   1.35030E-06   1.46345E-05   9.07423E-06   1.68110E-05
2.66753E-05
  0.355   1.51130E-05   2.15764E-05   1.23685E-05   1.73016E-05
2.39984E-05



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