"Too Many Input/Output Arguments" error for nrlmsise00 function

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Jacob
Jacob 2024 年 12 月 19 日
移動済み: Torsten 2024 年 12 月 19 日
I am trying too run a script that involves this function:
rho = nrlmsise00(altitude, year, month, day, hour, minute, second);
Every time I try to fix it, I get the same errors. If I reduce the input arguments, I get the too many input arguments error until I reduce it to nothing (then I get the too many output arguments error). I don't have the Aerospace toolbox, so I downloaded the nrlmsise00 function off of this site, and I don't know if it has been added to the path, but I tried every way to add it. What are your thoughts? Please help, thank you.
  2 件のコメント
Torsten
Torsten 2024 年 12 月 19 日
If you downloaded it here
you will see that the function has neither inputs nor outputs.
Jacob
Jacob 2024 年 12 月 19 日
@Torsten Yes, that is the one, but should I just put in the function by itself in my orbit propagation code? I'm trying to get a density out of it.

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採用された回答

Torsten
Torsten 2024 年 12 月 19 日
移動済み: Torsten 2024 年 12 月 19 日
The results for the defined testcase seem to coincide with what is stated in the Documentation (see below).
You will have to adapt the function nrlmsise00 according to your needs (which means you have to understand which data you have to supply (input structure) and which data you can get out of the function (output structure)) .
nrlmsise00()
6.665177E+05 1.138806E+08 1.998211E+07 4.022764E+05 3.557465E+03 4.074714E-15 3.475312E+04 4.095913E+06 2.667273E+04 1.250540E+03 1.241416E+03 3.407293E+06 1.586333E+08 1.391117E+07 3.262560E+05 1.559618E+03 5.001846E-15 4.854208E+04 4.380967E+06 6.956682E+03 1.166754E+03 1.161710E+03 1.123767E+05 6.934130E+04 4.247105E+01 1.322750E-01 2.618848E-05 2.756772E-18 2.016750E+04 5.741256E+03 2.374394E+04 1.239892E+03 1.239891E+03 5.411554E+07 1.918893E+11 6.115826E+12 1.225201E+12 6.023212E+10 3.584426E-10 1.059880E+07 2.615737E+05 2.819879E-42 1.027318E+03 2.068878E+02 1.851122E+06 1.476555E+08 1.579356E+07 2.633795E+05 1.588781E+03 4.809630E-15 5.816167E+04 5.478984E+06 1.264446E+03 1.212396E+03 1.208135E+03 8.673095E+05 1.278862E+08 1.822577E+07 2.922214E+05 2.402962E+03 4.355866E-15 3.686389E+04 3.897276E+06 2.667273E+04 1.220146E+03 1.212712E+03 5.776251E+05 6.979139E+07 1.236814E+07 2.492868E+05 1.405739E+03 2.470651E-15 5.291986E+04 1.069814E+06 2.667273E+04 1.116385E+03 1.112999E+03 3.740304E+05 4.782720E+07 5.240380E+06 1.759875E+05 5.501649E+02 1.571889E-15 8.896776E+04 1.979741E+06 9.121815E+03 1.031247E+03 1.024848E+03 6.748339E+05 1.245315E+08 2.369010E+07 4.911583E+05 4.578781E+03 4.564420E-15 3.244595E+04 5.370833E+06 2.667273E+04 1.306052E+03 1.293374E+03 5.528601E+05 1.198041E+08 3.495798E+07 9.339618E+05 1.096255E+04 4.974543E-15 2.686428E+04 4.889974E+06 2.805445E+04 1.361868E+03 1.347389E+03 1.375488E+14 0.000000E+00 2.049687E+19 5.498695E+18 2.451733E+17 1.261066E-03 0.000000E+00 0.000000E+00 0.000000E+00 1.027318E+03 2.814648E+02 4.427443E+13 0.000000E+00 6.597567E+18 1.769929E+18 7.891680E+16 4.059139E-04 0.000000E+00 0.000000E+00 0.000000E+00 1.027318E+03 2.274180E+02 2.127829E+12 0.000000E+00 3.170791E+17 8.506280E+16 3.792741E+15 1.950822E-05 0.000000E+00 0.000000E+00 0.000000E+00 1.027318E+03 2.374389E+02 1.412184E+11 0.000000E+00 2.104370E+16 5.645392E+15 2.517142E+14 1.294709E-06 0.000000E+00 0.000000E+00 0.000000E+00 1.027318E+03 2.795551E+02 1.254884E+10 0.000000E+00 1.874533E+15 4.923051E+14 2.239685E+13 1.147668E-07 0.000000E+00 0.000000E+00 0.000000E+00 1.027318E+03 2.190732E+02 5.196477E+05 1.274494E+08 4.850450E+07 1.720838E+06 2.354487E+04 5.881940E-15 2.500078E+04 6.279210E+06 2.667273E+04 1.426412E+03 1.408608E+03 4.260860E+07 1.241342E+11 4.929562E+12 1.048407E+12 4.993465E+10 2.914304E-10 8.831229E+06 2.252516E+05 2.415246E-42 1.027318E+03 1.934071E+02 DAY 172 81 172 172 172 UT 29000 29000 75000 29000 29000 ALT 400 400 1000 100 400 LAT 60 60 60 60 0 LONG -70 -70 -70 -70 -70 LST 16 16 16 16 16 F107A 150 150 150 150 150 F107 150 150 150 150 150 TINF 1250.54 1166.75 1239.89 1027.32 1212.40 TG 1241.42 1161.71 1239.89 206.89 1208.14 HE 6.665e+05 3.407e+06 1.124e+05 5.412e+07 1.851e+06 O 1.139e+08 1.586e+08 6.934e+04 1.919e+11 1.477e+08 N2 1.998e+07 1.391e+07 4.247e+01 6.116e+12 1.579e+07 O2 4.023e+05 3.263e+05 1.323e-01 1.225e+12 2.634e+05 AR 3.557e+03 1.560e+03 2.619e-05 6.023e+10 1.589e+03 H 3.475e+04 4.854e+04 2.017e+04 1.060e+07 5.816e+04 N 4.096e+06 4.381e+06 5.741e+03 2.616e+05 5.479e+06 ANM 0 2.667e+04 6.957e+03 2.374e+04 2.820e-42 1.264e+03 RHO 4.075e-15 5.002e-15 2.757e-18 3.584e-10 4.810e-15 DAY 172 172 172 172 172 UT 29000 29000 29000 29000 29000 ALT 400 400 400 400 400 LAT 60 60 60 60 60 LONG 0 -70 -70 -70 -70 LST 16 4 16 16 16 F107A 150 150 70 150 150 F107 150 150 150 180 150 TINF 1220.15 1116.39 1031.25 1306.05 1361.87 TG 1212.71 1113.00 1024.85 1293.37 1347.39 HE 8.673e+05 5.776e+05 3.740e+05 6.748e+05 5.529e+05 O 1.279e+08 6.979e+07 4.783e+07 1.245e+08 1.198e+08 N2 1.823e+07 1.237e+07 5.240e+06 2.369e+07 3.496e+07 O2 2.922e+05 2.493e+05 1.760e+05 4.912e+05 9.340e+05 AR 2.403e+03 1.406e+03 5.502e+02 4.579e+03 1.096e+04 H 3.686e+04 5.292e+04 8.897e+04 3.245e+04 2.686e+04 N 3.897e+06 1.070e+06 1.980e+06 5.371e+06 4.890e+06 ANM 0 2.667e+04 2.667e+04 9.122e+03 2.667e+04 2.805e+04 RHO 4.356e-15 2.471e-15 1.572e-15 4.564e-15 4.975e-15 DAY 172 172 172 172 172 UT 29000 29000 29000 29000 29000 ALT 0 10 30 50 70 LAT 60 60 60 60 60 LONG -70 -70 -70 -70 -70 LST 16 16 16 16 16 F107A 150 150 150 150 150 F107 150 150 150 150 150 TINF 1027.32 1027.32 1027.32 1027.32 1027.32 TG 281.46 227.42 237.44 279.56 219.07 HE 1.375e+14 4.427e+13 2.128e+12 1.412e+11 1.255e+10 O 0.000e+00 0.000e+00 0.000e+00 0.000e+00 0.000e+00 N2 2.050e+19 6.598e+18 3.171e+17 2.104e+16 1.875e+15 O2 5.499e+18 1.770e+18 8.506e+16 5.645e+15 4.923e+14 AR 2.452e+17 7.892e+16 3.793e+15 2.517e+14 2.240e+13 H 0.000e+00 0.000e+00 0.000e+00 0.000e+00 0.000e+00 N 0.000e+00 0.000e+00 0.000e+00 0.000e+00 0.000e+00 ANM 0 0.000e+00 0.000e+00 0.000e+00 0.000e+00 0.000e+00 RHO 1.261e-03 4.059e-04 1.951e-05 1.295e-06 1.148e-07

その他の回答 (1 件)

Walter Roberson
Walter Roberson 2024 年 12 月 19 日
The nrlmsiese00 function at https://www.mathworks.com/matlabcentral/fileexchange/56253-nrlmsise-00-atmosphere-model does not accept any inputs and does not produce any outputs.
Instead of inputs, you need to adjust the values in the lines
flags = struct('switches',zeros(24,1),'sw',zeros(24,1),'swc',zeros(24,1));
ap_a = struct('a',zeros(7,1));
input = struct('year',0,'doy',0,'sec',0,'alt',0,'g_lat',0,'g_long',0,'lst',0,'f107A',0,'f107',0,'ap',0,'ap_a',ap_a);

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