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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
6 i0 n/ y' a. Lexpecting one of the end of statement, 到底错在哪里啊，求助一下！！！！# J2 g. x( n9 X( ?& M% Y# ] N
程序如下8 y7 x7 W8 Y+ m! d6 K
SUBROUTINE AC8B(MC,ISLOT)
: A7 O/ A5 r, w7 Z6 A/ ~$ W INTEGER MC,ISLOT 4 l- c; C4 W t( |8 z
C 8 p' n: u L% @& K3 b
C MC =MACHINE ARRAY INDEX . o; Q/ [ l3 ]1 x$ h m
C ISLOT=ARRAY ALLOCATION TQABLE INDEX + j3 u. j- t0 p+ y v
C J =STRTIN(1,ISLOT) [USES CON(J) THROUGH CON(J+20) ] 8 @4 i+ c0 n7 V* v6 ^
C K =STRTIN(2,ISLOT) [USES STATE(K) AND STATE(K+4) ] / S2 z ~3 M9 D; W; j2 A4 d9 n
C 0 u+ J( ~" G. p3 O: M! d
$INSERT COMON4 & O0 @# a+ ?% J; X2 d" l9 W
C
$ T( R* z4 H& ^0 p) f: t$ f INTRINSIC MAX, EXP, LOG
5 N, J3 r' D/ |, L EXTERNAL BADMID ' U! O0 E8 q. v
C 6 H) ?* j4 {0 X" I
INTEGER IB, J, K
0 Y; R; w H k: F- j4 D1 g0 K REAL VERROR, VPID, SE, IN, FEX, VEMAX, A, B/ F0 P: X8 f0 i6 u* k
REAL VE0, VR0, VPID0
U. j; c {: J4 U5 iC
V9 B1 o) r' @- Z' ?" e1 J) V* JC DO NOTHING IN ACTIVITIES 'DOCU' AND 'DYDA' FOR NOW & l" X0 K5 K5 R' S! e/ O* Z! N
C X! N( O9 s2 O0 s2 o3 ~! X0 E
IF (MODE.GT.4) RETURN 9 l6 C+ L5 ~2 h' J" C
C
# ?. ?! z: H8 ^/ u( b$ pC BUS SEQUENCS NUMBER NEGATIVE IF MACHINE # U+ w. T1 V8 L3 Q% x$ S6 J1 v* Y {
C IS OFF LINE,SVS OR INDUCTION MACHINE 5 N, H2 y! e1 {7 {
C * l: g' W% `6 }- u
IB=NUMTRM(MC)
' i% ]1 ~ ~1 u6 F' D# j IF (IB.LE.0) RETURN 2 V: f! k2 G3 A; d9 F- _" k
C / T+ W; O- t" T7 O
IF (MIDTRM) GO TO 900
/ l* r$ _* R N1 f" f6 lC
o' I& {% i: M4 N, sC GET STARTING 'CON' AND 'STATE' INDICES ' ?* T- \% g$ b
C / z$ g% Z7 Q6 p: b# w0 H* ]2 U8 e
J=STRTIN(1,ISLOT)
0 t, k3 d5 s+ z* G1 x2 u K=STRTIN(2,ISLOT)- Q# m; c5 [( w+ ?6 g: d6 a' Z
B=LOG(CON(J+20)/CON(J+18))/(CON(19)-CON(17))
9 @; a6 b! u5 S C" `% ~ A=CON(J+18)/EXP(B*CON(J+17))
0 T, S7 o$ w9 Y- k7 WC $ \! H& _! m% ~4 |2 O U+ P4 }
GO TO (100,200,300,400),MODE
8 |: M& I9 l, C7 g, ZC
: D, k4 m2 L8 j8 ?2 u4 z4 z8 }C MODE = 1 – INITIALIZE
& Z; U& _& m- {+ V) G9 |( h5 CC
% U3 n8 H5 Z1 W- y8 A100 STATE(K)=ECOMP(MC) |* v/ i4 F$ Q: E4 w# D e
VREF(MC)=ECOMP(MC)-VUEL(MC)-VOEL(MC)
. Q0 J9 f6 k$ H STATE(K+2)=0
$ p3 v$ u: m: g/ i0 X* N: _ VE0=EFD(MC)+0.577*CON(J+11)*XADIFD(MC)
6 Z- K2 T" c# C& K( y VR0=(A*EXP(B*VE0)+CON(J+13))*VE0+CON(J+12)*XADIFD(MC)3 G+ U3 [1 Y0 a( }! r
VPID0=VR0/CON(J+7)
9 t6 |/ Y* W+ x. k; x5 m/ o STATE(K+4)=VE0
7 \& H, z t9 F3 K STATE(K+3)=VR03 q. B: ^/ H1 y1 g8 B2 P0 c
STATE(K+2)=VPID0# A) a: m5 P* @2 K( Z; X
VAR(L)=VPID0
! s2 o: u. ^3 ~1 Q f VAR(L+1)=1-0.577*XADIFD(MC)/VE0
, Q, }& H; z% J VAR(L+2)=(CON(J+15)-CON(J+12)*XADIFD(MC))/(CON(J+13)+A*EXP(B*VE0))
) D" A, q8 z I H IF (VR0.LT.CON(J+10).OR.VR0.GT.CON(J+9)) THEN 9 n9 l; r3 q0 J3 |# n
WRITE(LPDEV,307) NUMBUS(IB),MACHID(MC)3 c6 Q* q3 Q6 N" k& e( N
ENDIF% W, \ }) w, ^) e& r
IF (VE0.LT.CON(J+16).OR.VE0.GT.VAR(L+2)) THEN 3 p/ l5 t; u+ V, y5 \
WRITE(LPDEV,307) NUMBUS(IB),MACHID(MC)
; r- r+ C6 b$ d# v, H: V X ENDIF# @; X, n: d1 C5 x: k
RETURN
( d& e9 N0 s- {! R7 t8 jC 3 A! j$ }2 c( Q
C MODE = 2 – CALCULATE DERIVATIVES - i& H/ W- Z4 n8 ]# d( k- Q* \
C 7 L; ?6 F. i! ?3 h+ Y
200 DSTATE(K)=(ECOMP(MC)-STATE(K))/CON(J)
t) ?9 n6 S2 F VERROR=VREF(MC)+VOTHSG(MC)+VUEL(MC)+VOEL(MC)-STATE(K)
; p2 L3 X3 n0 A0 L. |$ d F8 _. [ DSTATE(K+1)=CON(J+2)*VERRROR e" ^) r' }0 }1 v) h- t
DSTATE(K+2)=(CON(J+3)/CON(J+4)*VERRROR-STATE(K+2))/CON(J+4)
! w; S$ z' Q% `# O5 e K5 l- s- A VPID=STATE(K+1)-STATE(K+2)+(CON(J+1)+CON(J+3)/CON(J+4))*VERROR
, U4 f3 n1 s1 w {& b IF(VPID.GT.CON(J+5)) VPID=CON(J+5)
9 D; E1 r9 @% Q4 G IF(VPID.LT.CON(J+6)) VPID=CON(J+6)# a6 g+ L) Z* R9 I
DSTATE(K+3)=(CON(J+7)*VPID-STATE(K+3))/CON(J+8). f- m: _1 k: U& P. n
IF(STATE(K+3).GT.CON(J+9)) STATE(K+3)=CON(J+9). }5 m5 N8 e6 }! J% V/ f
IF(STATE(K+3).LT.CON(J+10)) STATE(K+3)=CON(J+10)
* s& O1 g% G- E. ^! E$ k4 k SE=A*EXP(B*STATE(K+4))
# |8 k7 j) v. i' l- q DSTATE(K+4)=(STATE(K+3)-(SE+CON(13))*STATE(K+4) - H: @% ~- s1 `( A+ E
* -CON(J+12)*XADIFD(MC))/CON(J+14)
' R1 V- S) u$ A' G# i; f VEMAX=(CON(J+15)-CON(J+12)*XADIFD(MC))/(CON(J+13)+SE)' e* g1 ]. d* b, G$ i& R' [$ \, R
IF(STATE(K+4).GT.CON(J+9)) STATE(K+3)=CON(J+9)
. Z. F/ m) J- w S3 c }( B IF(STATE(K+4).LT.CON(J+16)) STATE(K+3)=CON(J+16)* n4 P+ e6 J3 N+ l9 Z
RETURN / M) U. }8 f! E. m
C 8 W- E& r4 V" D
C MODE 3 – SET EFD
1 u% l5 Y- L2 F$ o! E$ \: w! F# CC - `! _' |8 F! k5 w% d y) o- e
300 IN=CON(J+11)*XADIFD(MC)/STATE(K+4), E) l- {: f/ Y0 A
IF(IN.LE.0) THEN
: A: }5 @5 a. I: f2 x+ z FEX=1
- W1 `6 f% v% P2 u, o& w7 | ELSEIF(IN.LE.0.433) THEN$ K h f; Y+ Z; M J
FEX=1-0.577*IN' \" ?6 T% x6 }4 {/ y5 m
ELSEIF(IN.LT.0.75) THEN @2 Y, A0 g: \& @* m/ ~! E. O0 }7 d
FEX=SQRT(0.75-IN*IN): R3 v' x- ` I8 N2 r* n
ELSEIF(IN.LE.1) THEN% z) @3 |' Y; _3 x( t
FEX=1.732*(1-IN) e) S3 {: R- Z
ELSE0 R8 B" Z! S6 Z% ~) E U7 s
FEX=0
, P; w. J, ~/ y% s8 I4 ] ENDIF
( w; f2 c; m0 B5 x" J& Z) `$ Q5 V- } EFD(I)=FEX*STATE(K+4)6 L. S$ w! g$ M! V+ a& Y
RETURN5 Y3 J1 e0 Y2 q8 u# Y+ u- Y: {
C
. n) ~; D: H2 LC MODE = 4 – SET NINTEG : D0 M! \2 W* v5 P* L9 `6 H$ c# L. p
C
+ B; R# Q" t* |6 I4 g+ p400 NINTEG=MAX(NINTEG,K+1) " \5 F3 t u. E+ B3 @, g0 i
RETURN
) }6 ] v( F& E" g2 k" B/ |C
! x4 f0 a* i9 ^5 {C MODEL NOT IMPLEMENTED FOR MSTR/MRUN0 b. w" t) t/ i; h' G% r
C
+ Q& K; \+ I+ v7 W& p307 FORMAT('AC8B AT BUS',16,'MACHINE',A,
2 J* N3 f4 ]. c3 l * , 'INITIALIZED OUT OF LIMITS')7 P3 I% {) G8 Z3 C x) h6 B' ^9 V
C: _" u6 x) A, |! n6 z/ U% {2 O
900 CALL BADMID(MC,IB,'AC8B')
. r' Y" t1 [4 u# P n7 W4 u RETURN
0 s* k7 K Q+ RC
0 Z7 M) Z \& ~" U6 D- \ END |
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