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: X- T. `; M6 S) Y G$ u4 L求助, 4 ?8 \4 M8 x7 s; i/ S9 u# ^# x
相关代码:
+ i4 k0 D; R# u/ jq=(r.*cos(e)./(r+h)).^2;
/ L6 ^, e; ]3 ~0 e, Z4 u& Q, n- }6 bam=1-q; : h! N1 Y* N0 U4 c# Y: z7 [ q
obliquity_factor=sqrt(am);%MF=stec/vtec 此时MF=1/obliquity_factor 6 p& m4 A8 i% h6 \$ w5 L, ?1 B4 \
MF=1./obliquity_factor;
9 K9 m; Y4 \$ `1 q" j" h: D! e0 [5 s% `& s5 p
Orbit_15degree=[]; ( L- r' ~/ Z/ Z3 ?- \
for i=1:length(Orbit_15min)
8 }8 ^3 x2 b/ t+ F7 O$ l for j=1:length(Sat_15degree)
5 |4 A9 u2 Z; K! e8 T if Orbit_15min(i,:)==Sat_15degree(j,:)
- c% P# ` W8 W; l" w Orbit_15degree_temp=Sat_15degree(j,:);
* F4 z8 b6 }, ^2 \ Orbit_15degree=[Orbit_15degree;Orbit_15degree_temp];
8 n9 y3 H# Q! a3 \& A: u end
1 d [1 d6 w6 R! `, |7 A. r. w6 f) r end
! n5 P1 L: A/ m; k" b Iend ( h! G. Y# _3 m) H' g
%15degree时的STEC
: L! H, i# {0 c/ X8 VKSsat_15deg=[];
& r6 e) w5 R$ i5 rfor j=1:length(Sat_15degree)
" ^ G( w0 ~! u) B; B9 e% B! _ for i = 1:size(KESATzong,1)
4 i* @( o2 G8 {% i( O if Orbit_15degree(j,:)==Orbit(KESATzong(i,3)).Coord(KESATzong(i,2),:)
# n" C' O- ^2 @ KSsat_15deg_temp=KESATzong(i,:);
$ c& M, b" z( P) i6 \' e KSsat_15deg= [KSsat_15deg;KSsat_15deg_temp]; / a9 j' k: X+ {# R# ~
end C8 s8 B1 b& R/ b9 F
end
0 A6 W8 }6 Q( E" c+ Eend
$ r4 a( h+ l( _4 e1 w' W. f( u( cVTEC=KSsat_15deg(:,4).*obliquity_factor;%每个可视卫星对应时刻IPP点处的VTEC 0 K* _4 V; P8 S' A+ w# M' g1 @
kssatzong=[KSsat_15deg, Orbit_15degree,e,B,CarA,LLipp,VTEC,MF]; 1 N7 N$ Y" o$ L% O+ X% n
+ h5 {$ L5 ?% `( Q2 @报错: 位置 2 的索引超出数组范围。
' F; v0 B; _% u6 c4 k
) z7 V4 P1 b8 Y0 ]
# n8 N# P+ {0 g$ i+ `5 {出错 IPPzuobiao (line 136)
" d: c) f4 v/ m4 J' X6 p: aVTEC=KSsat_15deg(:,4)*obliquity_factor;%每个可视卫星对应时刻IPP点处的VTEC ) {2 Q* d0 o2 O5 d* Q
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