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0 ?, {- o/ V$ }4 _& |求助, ) ^2 t1 I! \% V
相关代码:
8 U8 y V2 j) I9 ?$ t/ w, H# hq=(r.*cos(e)./(r+h)).^2; 9 Y; r- X0 y! r& F
am=1-q; ( C+ V7 K; o; X6 a' i2 G# a, |
obliquity_factor=sqrt(am);%MF=stec/vtec 此时MF=1/obliquity_factor
% r4 y0 @3 l' J K, ]$ QMF=1./obliquity_factor; / o1 J7 Z1 P/ J* L/ E& r) N
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Orbit_15degree=[]; , y7 Y M* S3 w2 V! H. a
for i=1:length(Orbit_15min) % @( z7 X: L0 D1 ~; L
for j=1:length(Sat_15degree) * _" w" I9 A$ b1 o- V
if Orbit_15min(i,:)==Sat_15degree(j,:) 2 W! B+ t2 m* V
Orbit_15degree_temp=Sat_15degree(j,:); 3 m0 {5 @/ \* w, E! O
Orbit_15degree=[Orbit_15degree;Orbit_15degree_temp];
, j0 l; ]1 I' S9 m/ o6 q end 8 D% r' l, b2 ?# U, _/ b9 o
end : j, D& v* J& q# m
end
7 N% t1 r% r# k# Z* Q! e, ?, I S3 Z0 m%15degree时的STEC
$ g: G" q' N' O- bKSsat_15deg=[]; M/ m5 e9 Q! {3 {2 ^) ^
for j=1:length(Sat_15degree) / A$ R" C5 M0 @5 e
for i = 1:size(KESATzong,1)
- m* [% w/ R7 K2 o if Orbit_15degree(j,:)==Orbit(KESATzong(i,3)).Coord(KESATzong(i,2),:)
. `. H: i6 _% R: T* }; L- U u KSsat_15deg_temp=KESATzong(i,:);
9 P8 }% `! c, u KSsat_15deg= [KSsat_15deg;KSsat_15deg_temp];
5 I$ V# |5 ~5 l1 F7 [% |, G end
+ X/ G' l3 e: q8 r" I+ E$ ] end 2 b+ Z* x. A3 @+ K
end
) j$ J# }' i! V, x" x' `7 ^% s$ eVTEC=KSsat_15deg(:,4).*obliquity_factor;%每个可视卫星对应时刻IPP点处的VTEC
# A( ~8 x& n$ l6 Q+ [1 m' y& A A9 \% akssatzong=[KSsat_15deg, Orbit_15degree,e,B,CarA,LLipp,VTEC,MF]; 5 E2 Y' e5 N2 D& I3 p, i
6 L' V1 ?$ p8 D a" I2 ^报错: 位置 2 的索引超出数组范围。 9 b; b: f+ a5 J6 A6 W+ x
( [! @! \# n0 R1 O* t5 [
7 Y" R! S6 X& S3 M$ Y: {6 ^" N& e出错 IPPzuobiao (line 136) % P) f0 _+ p# x2 R, ]
VTEC=KSsat_15deg(:,4)*obliquity_factor;%每个可视卫星对应时刻IPP点处的VTEC
( N2 z9 H) w- h" |( W9 f# w; U1 j9 k5 t. e: \2 y6 \* \1 e0 F
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