|
|
马上加入,结交更多好友,共享更多资料,让你轻松玩转电力研学社区!
您需要 登录 才可以下载或查看,没有账号?立即加入
×
请教一下各位大神,我的AC8B自定义模型程序总是通不过编译报错END STATEMENT IS MISSING,Syntax error found identifier strtin when ( R* V! T( s, c0 p+ V5 @
expecting one of the end of statement, 到底错在哪里啊,求助一下!!!!
" |1 k; e- d# b8 _+ B程序如下
+ |* t% y. h7 T' x X" n, WSUBROUTINE AC8B(MC,ISLOT)
9 X; @% w7 g& L INTEGER MC,ISLOT 6 U0 C/ s8 t. |
C : F. l8 `, W7 D! n# D. W
C MC =MACHINE ARRAY INDEX 1 ^; x8 F. `& k0 ]
C ISLOT=ARRAY ALLOCATION TQABLE INDEX , q2 _! m9 N& e% g9 D5 @. ?
C J =STRTIN(1,ISLOT) [USES CON(J) THROUGH CON(J+20) ] 0 N, |- r2 @' |) [
C K =STRTIN(2,ISLOT) [USES STATE(K) AND STATE(K+4) ]
1 Z1 t3 s! _% F* Z6 eC
. W5 X& R& n. b# w; u $INSERT COMON4 - }" Z4 c3 b1 Z( }/ O$ R8 Q* \5 v7 z
C
) W( j( t3 s4 v INTRINSIC MAX, EXP, LOG ' r( X0 o/ V# w- p9 K. d
EXTERNAL BADMID
; R# J" v m3 R3 nC
: G# s& H8 D4 m INTEGER IB, J, K 5 ^ }+ Q$ y6 |6 M. h
REAL VERROR, VPID, SE, IN, FEX, VEMAX, A, B/ T" }1 S* n6 S& ?; ~
REAL VE0, VR0, VPID0$ e1 C4 S1 ?2 ~
C " {: a- b4 v" Q# g- t( k+ ?
C DO NOTHING IN ACTIVITIES 'DOCU' AND 'DYDA' FOR NOW % L4 d6 Q. I) Z' w6 k2 X
C
# X+ h; N8 E% B, k6 j IF (MODE.GT.4) RETURN / A! K/ W0 z' m7 r1 ^
C ) n @. E K& j# g& _% b3 z/ R7 c5 a
C BUS SEQUENCS NUMBER NEGATIVE IF MACHINE " l7 M7 T, I! y# ]; b
C IS OFF LINE,SVS OR INDUCTION MACHINE ' g' d& n. W# X' c2 S
C
( ~: P, {% K8 h& d: n& F IB=NUMTRM(MC) $ t- l% b9 Y1 K6 b q2 v0 c
IF (IB.LE.0) RETURN 1 l. w: k, ~+ D6 m% s( V" c5 s
C . K. ?% i8 y, @% B9 b, Q2 _8 ?
IF (MIDTRM) GO TO 900
7 Z4 N' d: `, u! jC 1 V1 b- f8 P/ T# k7 @+ o, u
C GET STARTING 'CON' AND 'STATE' INDICES
6 R% I: [1 _9 p# G! [7 `; ]C 2 O: w k0 X: ?$ B& D6 B0 k( C* o; d
J=STRTIN(1,ISLOT) ; C! n5 D' q$ Q& Q! d- m. L; h
K=STRTIN(2,ISLOT)
, u0 G* D1 G) v) r B=LOG(CON(J+20)/CON(J+18))/(CON(19)-CON(17))
, H8 c( `* {# w# T& A$ | A=CON(J+18)/EXP(B*CON(J+17))
" M& Z- u" L# Z! ] B. M( o) l2 m* sC
0 m2 l1 F4 Q1 W% ~! j4 x GO TO (100,200,300,400),MODE
9 Y: s$ H( u* t9 a$ v" ~C ( U0 q( }( y, ^
C MODE = 1 – INITIALIZE
$ h& r( F4 a2 C9 BC
$ S, d4 [7 V3 ?8 l100 STATE(K)=ECOMP(MC)
9 ]$ I+ h6 C( Z7 X6 | VREF(MC)=ECOMP(MC)-VUEL(MC)-VOEL(MC)
; {: X9 x: L/ n9 M* ^ STATE(K+2)=0 G( o) Y# f$ E) J" L* J8 N8 T% l0 Z; [6 p
VE0=EFD(MC)+0.577*CON(J+11)*XADIFD(MC)
# |3 `0 j6 T# g* S% D VR0=(A*EXP(B*VE0)+CON(J+13))*VE0+CON(J+12)*XADIFD(MC)
6 J5 J F" J7 n& q) u VPID0=VR0/CON(J+7)
' E7 E# s+ D: `, p0 r STATE(K+4)=VE0+ Q& b Z" h7 _- R5 v
STATE(K+3)=VR0
6 r/ L9 O, u7 R3 i& X' J STATE(K+2)=VPID0" J; x% Z" C! N1 ^. u1 g% n
VAR(L)=VPID0. p- W1 f1 g& R; t. p& I
VAR(L+1)=1-0.577*XADIFD(MC)/VE0, M$ H! d. b7 P7 M' X0 R7 G3 f
VAR(L+2)=(CON(J+15)-CON(J+12)*XADIFD(MC))/(CON(J+13)+A*EXP(B*VE0))) }7 e0 C, v2 a: L/ e$ h- c2 K
IF (VR0.LT.CON(J+10).OR.VR0.GT.CON(J+9)) THEN
L; z; Z2 V5 O WRITE(LPDEV,307) NUMBUS(IB),MACHID(MC)! n# c5 d( c2 z. Z1 m T( s7 W
ENDIF* }4 y% T" b9 [$ s2 D
IF (VE0.LT.CON(J+16).OR.VE0.GT.VAR(L+2)) THEN m! O+ M2 ~, w: x" c% y/ k; {
WRITE(LPDEV,307) NUMBUS(IB),MACHID(MC)
6 _! m& v2 z2 _4 q/ j6 A ENDIF
- ]' ?+ q# Y* V+ S2 G RETURN 3 q/ }$ v! I( v2 G
C 1 z; z3 _9 V# }6 f' X
C MODE = 2 – CALCULATE DERIVATIVES
% j% r+ I; e, m2 rC ( U$ v& H' [6 N3 Y! v8 @) j
200 DSTATE(K)=(ECOMP(MC)-STATE(K))/CON(J) 3 W' `" ]: r( |* ~, q. x+ v+ }
VERROR=VREF(MC)+VOTHSG(MC)+VUEL(MC)+VOEL(MC)-STATE(K) 4 T5 \( x j. d2 h
DSTATE(K+1)=CON(J+2)*VERRROR
- O! x! O6 y6 u" v2 J1 Z DSTATE(K+2)=(CON(J+3)/CON(J+4)*VERRROR-STATE(K+2))/CON(J+4)& F( p+ K3 |5 h
VPID=STATE(K+1)-STATE(K+2)+(CON(J+1)+CON(J+3)/CON(J+4))*VERROR4 r c* v0 ~- Z: q: v
IF(VPID.GT.CON(J+5)) VPID=CON(J+5)6 N! M6 p* |8 L; O* Y4 u& I0 u7 f
IF(VPID.LT.CON(J+6)) VPID=CON(J+6)
: }7 ]2 m/ f U: E: n DSTATE(K+3)=(CON(J+7)*VPID-STATE(K+3))/CON(J+8)
; [) r$ Q! V8 t) i" l9 }0 F IF(STATE(K+3).GT.CON(J+9)) STATE(K+3)=CON(J+9)
1 u4 P, o- e8 j Y IF(STATE(K+3).LT.CON(J+10)) STATE(K+3)=CON(J+10)
3 {: M+ m, t1 H SE=A*EXP(B*STATE(K+4))
: O- A7 Q1 R: ]) L/ { DSTATE(K+4)=(STATE(K+3)-(SE+CON(13))*STATE(K+4) 4 I/ f! L6 i$ S) a6 p8 ~5 W
* -CON(J+12)*XADIFD(MC))/CON(J+14)( ?* z# R7 j- k. S0 J: f0 h8 G, T
VEMAX=(CON(J+15)-CON(J+12)*XADIFD(MC))/(CON(J+13)+SE)1 R6 P. a b) V3 K( F. X
IF(STATE(K+4).GT.CON(J+9)) STATE(K+3)=CON(J+9)
$ v% Y& I( r2 a: i# q IF(STATE(K+4).LT.CON(J+16)) STATE(K+3)=CON(J+16)
" j M* d8 `- ? RETURN ) x; V+ P2 w2 Y$ E- P
C
1 I* o2 z$ C8 J, H2 M UC MODE 3 – SET EFD
; G2 Q Q" p% c8 K' L# p, W$ U# YC . o1 h# J P! B! Q0 t, A& m0 v
300 IN=CON(J+11)*XADIFD(MC)/STATE(K+4)
@& @$ p/ v" i! S IF(IN.LE.0) THEN
, [2 ^$ s% |" x" D0 a! d FEX=1' k( D7 e+ {( x' r" ^0 B0 J% }
ELSEIF(IN.LE.0.433) THEN$ G! y9 q* K/ b8 O2 W
FEX=1-0.577*IN% Z+ w, I; R2 M6 m$ ? N: g3 _* `
ELSEIF(IN.LT.0.75) THEN1 D. ^9 f7 T2 v, d, e: x
FEX=SQRT(0.75-IN*IN)
7 _' s: Z/ j' h7 @( t% Y ELSEIF(IN.LE.1) THEN
8 k; ]& m" {& j# k( T4 t* E. F FEX=1.732*(1-IN)
( Q) Q1 g3 S4 ]( } ELSE
1 f8 n+ X. V& \. @ FEX=0
% H3 k' C: |' H0 I ENDIF
+ S7 L+ l4 ~( K4 M) r9 `) ~" _ EFD(I)=FEX*STATE(K+4)
) f1 k$ Q7 g- J/ V, b6 F RETURN3 W5 J" x- U7 v/ v, A
C
* X5 u) Y+ X" p7 D; o7 {C MODE = 4 – SET NINTEG
( s* d5 L, a( c: ? GC
$ p, u! f l% }0 ^2 Y: O' o) M400 NINTEG=MAX(NINTEG,K+1)
9 K$ l0 R: ~3 b' Y" B* ` RETURN0 p( _" l4 n. @2 d, g8 s
C ! S. \, q# c% a
C MODEL NOT IMPLEMENTED FOR MSTR/MRUN
2 V3 i7 ?, x$ i$ k6 @C
3 ?0 k9 h4 Z7 V) j307 FORMAT('AC8B AT BUS',16,'MACHINE',A,
' o' y* t' N Q; {0 s6 @* c" h * , 'INITIALIZED OUT OF LIMITS')1 Y( U" K7 h3 ~
C
5 d) h. d1 ]. ~2 A: \ }900 CALL BADMID(MC,IB,'AC8B')1 w3 A& [8 q ?8 e1 K
RETURN
( e( x3 Q# B2 m' u$ Y2 w9 H2 @C
+ a/ Q f. f2 m* b- C- k4 P% w END |
|