UntitledINTRODUCTION
w CREW SYSTEMS
issued. Small revisions to individual drawings, pleahee
figures, tables, or notes will be published as TATION
drawing change notices (DCN's) and/or page change
1notices (PCN's) as required. 10 GUIDANCE AND
CONTROL
This cover revised by Change 4, dated June 2, 1969.
T - O T
DISPLAY DWGS
DISPLAY SWITCHING
LGC OUTPUT INTERFACE
DWG 10.11 (SHT 1 OF 2)
DWG 10.11 (SHT 2 OF 2)
MIT SIGNAL CONDITIONING
DWG 10.13 (SHT 1 OF 2)
PGNS C&W HARDWAREINTERFACE
RENDEZVOUS RADAR SIGNAL FLOW
LANDING RADAR SIGNAL FLOW
DWG 10.16 (SHT 1 OF 2) DWG 10.16 (SHT 2 OF 2)
ORDEAL
|
DWG 10.17 DWG 10.17.1
DWG 10.17.3
AEA SOFTWARE
DESCENT ENGINE DWG 1020.2 SIGNAL FLOW AMPLIFIER 1 DWG 10.21
DWG10.20.3
ASCENT ENGINE SIGNAL FLOW
TW SU
SA IN
N WI
2 G& ‘AERONAUTICS & SPACE ADMINISTRATION
SPACECRAFT CENTER - TEAS
@ Rp
@ {3
RADAR
NDZ Quan 4 S-BAND
SL ; J?
PGHS TOTAL ATTITUDE
VELOCITY TRACKER LOCK VEL DATA Good
RNG DATA GOOD ALTIMETER FREQUENCY DATA TRACKERS comurer [to
SELF TEST RANGE TRACKER LOCK ‘CIRCUIT
LR SELF TEST
SELF TEST ‘cIRCUIT
‘TRACKER TRACKER Lock DATA GOOD RNDZ RADAR
‘CAUTION PNL2 e0s28
GG2219¥ GG2249v GG2279v
yTAL ATTITUDE (RSVR OUTPUTSSIN IX COS DX) AC BUS A
vi
Ie ix rsye MG 1K RSVR 0G 1x RSVR’ SIN, COSSIM, COS
G2112v Goc72v 662113 6c2143v scai73v
FLIGHT DISPLAYS
cos Ix
IMU CAGE
cage OVERRIDE
Ze 10,3
C/A RELAYS
PART OF Pwr
PGKS VELOCITY
ISS WARNING Go9002x 60510
eec RCDU FAIL DISPLAY ELECTRONICSINERTIAL 28 voc
teu (3)
HEATERS.
15S COU ZERO(2)
Lec operate @G1523x
CH 15 BITS 1-5 cH 10 BITS 1-15 nai BITS 1-7 cw 12 817 13,14
cH 1487S 11,12
cH 128IT 8
cH 14.BIT 2
cH 30817 15
428 VOC
cH 308IT 1 CH 30BIT 3 cH 32817 9
‘cH 32817 10 cH 30BIT 5 cH 30BIT 10
GH 31 BITS 7,9,11 cH a1 (cH 31 14 ch 31 BIT 13 on 31 BIT 15
cH 31 BITS 1-6
cH 11 BIT 13
cH 11 BIT 14
cH 1z BITS 9-12
} To ses
agi
428. voc swircHING aZs
2 RATE DESCENT RATE RESET ROMRATE OF DESCENT -1 FPS DESOENT RATE STEN ASS EAES
LAT VELOCITY RATE
FROM ABORT SWITCH, 1523, PRL 1 FROM ENG ARM SWITCH, 181, PHL 1 FROM ENG GIMBALSWITCH, 158, PRL 3 TO DECA (TRIM ELEC) FROM DECA TRIM MALFUNCTION ELEC FROM THROTTLE CONT SWITCH, 1811, PHLAUTO THRUST CMD
FROM GUIDANCE CONT SWITCH, 9S6, PNL 1 TO DECA (AUTO THROTTLE LOGIC)
x Trea’s
“X,Y, Z TRANSLATION CMOS FROM THROTTLE CONT SWITCH, 1521, PML 1
} ou MODE CONTROL STH,11524, PRL 3 FROM ACA TO PRIMARY PREAMPS (ATCA)
ATT ERROR
TOTAL ATT
0G IN hier] Tis vac 0G cos stone
La in ]
T
11 0s Ao cos AMG = | at sme 10 FOAAND{ |tettou {
YAW ANGLE ATTITUDE MONITOR
' t| 20s AMG sm | t ozs
1 I ! 1031 { | 1 siz
€ | ' ie :
nT 2B VAC 1> soon 00 Me | | i J @) t ! Jains caine +
{28 voe| ‘SIN pcos - cos aSIN'T
€ “SiN AKG /+28 voc
Ag SN
aevac atone pote 115 vac 2) ng oh
Ze we 10.710.7
Wa IN GD
TW NO LL WN |
3i vO
By al
‘N OL
sn OH
F E D v @ efocn] on [ENG Dare |APPROVAL c spl Aad P/zo/4 2/34 fo Gf em COMMENTS j
8 Z > 400 Nz coR FOAL toa |
400 Hz LMP FOAI 375> 108
TL FOTATES ABOUT 2 AKIS, SEEN AS fous venousROTATES atout 2am ROTATION ABOUT THE LINE OF VIEW
SPHERE DRIVE SYSTEM 1a¥oPAGED 2
ROLL
1804 dooce
|
|
sive view z
sim Coc) aoonz 10.4.2
BALL ROTATES ABOUT x AXIS, SEEN AS —J oRveaL con poe saw, VeMLe RoraTES anour canis FOTATION FROW SIDE.70SIDE
+ vAW “8
venicuepireh é fare 200 We ROLL OAC
10.20 enon RA eRROH POINTER were | ROLL (UPPER)
ee & 7)
sZs a yaw \— 1 ortzontaL 10.26 BEMnD, RATE ERROR POINTER
5 a - METER
vos Att veces " Ud aa
| Ze soo ke vaone | Oye 3 y
ine 3 ewtoo 3 pewoo ERROR POINTER { 3 yaw (LO
Bp tr 7 | + = =
1 Fr]
14
7
Ba 10.1 10,1
_
[oaTE eeeaES, taaNNEO SPACECRAFT CEN nouston. rexas [Eda eae
DSGN cleo ge setae) 769 1 FDAI [Seg “ NOTES: 1 BWG1S REPRESENTATIVEee OF BOTH FOAIS (9M2-2M6)
ma iG ND Litiifes Vere?
10.4.3 RUM AO ey Pe os UNIVERSAL
aaa. OSCILLATOR
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512 KHZ Po 45
aeae
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n sauna 2 J oe ie ii — sila cous. 995 cov ewes wie os |ue ae. one ; i ‘4
oe TIMING ~~ wa
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svoniea [8S] gw |liee eb |3.2 KPPS VZA GATE STROBE 2 1a 8 aR
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\|Ex
‘is s.avorsseser rssznsneserJosasizvorsneser
pressmse 08 2G) Lec ouTPUT 4c 3.2 PS nua care ts) _.()
snouses INTERFACE 10 sgumemaaieaie un © 3 P2wrsmuras 2 5)
Sania [ene] Toaoe PELTINTONres [oars] rome,eto rer eee bef Stan WTMN LGC SYNC D fl= NC AND TIMING —|
2 SIGNAL FLOW oe
o n
S. 5
FOR DETAILi a CLUTCH POSITION SEE OWG 10.20.8 JETS =CLOSED
THROTTLE = OPEN
AOT PANEL,
ESSey "Zs +28 voc
TTCA/TRANSL.
oR PML 3 us3
Loc RADAR
Mu CAGE
ANALOG ROTATIONAL CMOS
CLOSE CLOSE l
‘THRUSTER 13-15
Lc psy KEY RESET 103
KEY CODE 1 603
START STAGE PROG 558
14 vo < ay COARSE ERROR > 2V (30°) RRCOU FAIL FINE ERROR > 1V (0.7*) G05 (6 -y) <2V 166.4") READ CNTR UPLINE < 160 HZ
aavoc < av COARSE ERROR > 2v (30") FINE ERROR > 1V (0.7) (OS (8- 9) 2(66.4") READ CNTR UPLINE >160 HZ
00 #2 54< 14 5 IMU FAIL
MG SERVO ERROR > 3V {.166") FAIL DETECTION 0G SERVO ERROR > 3V 1.166") PITCHLO 242
PITCH ANALOG CMD 142
TEMP IN LIMIT
PITCH FAIL 3 camiore PITCH MALE
Lose
RR RADAR 7 RR RANGE. LO SCALE
15817 DATA ‘COUNTER
LANDING RADAR
ANTENNA ASSY
Lock ON
VELOCITY TRKR BEAM 3
yerrcurr
NOTES: THE 0 CIRCUIT INPUTS TO CHANNELS 15 AND 16 ARE NOT INVERTED AT THE INPUT REGISTER INTERFACE
iD START ACA
AciRcuT
NOTES: THE O CIRCUIT INPUTS TO CHANNELS 30, 31, 32, AND 3: ARE INVERTED AT THEINPUT REGISTER INTERFACE
circuit
CHANNEL 30 "ABORT
4X, #Y, 42 TRANS CMOS
Pipa FAIL
GIMBAL FAIL/OFF INBITS
UPLINK SERIAL DATA
‘CHANNEL 33
SCALER BINCR
cou z
ieou x
DRIVE SHT
DRIVE TRUN
RIVE x COU DRIVE ¥ COU DRIVE Z-COU DRIVE GYRO TIME 4 TIME 3
E MEMORY CNTRS
cou s COUNTER
PINBALL,
TO RADAR
AOT ROUTINES,
TO DAP LOG MONITOR ROUTINES AND T=4 RUPT Ea
TOCH BITS 13, 15 RESET UNDERFLOW
GyRo CMDS
3 ra Rupr
TO DAP ROUTINES
ROUTINES
Te Tocni3 eit 15 ser UNDERFLOW puPT OVERFLOW 75. |_TOOAP ROUTINES
ruPr yo HANO- |_LPo cmos
TRANS CMOS
‘To GUID ROUTINES
TO RADAR ROUTINES9 RADAR
ONLK ORDER BIT ACA.CHTR ENABLE START ACA READ
ENABLE T-6 RUPT ALT/ALT RATE CMDS THRUST CMOS
TRAP 31A,8,32 RESET CMDS START ACA READ ACA CNTR ENABLE T-o RUPT CMO GYRO ACT CMD SHT/TRUN COU DRIVE CMOS X/V/2 COU DRIVE CMOS RESET GYRO ACT
RESET RR ANO ISS COU DR aR AND ISS COU CMOS
GvR0 CMOS:
1 THIS DRAWING DEPICTS FUNCTIONAL SYSTEM FLOW ONLY AND IS NOT TO BE USED AS A DETAILED SCHEMATIC
0OLGC1 SIGNATURES DATE
L6c INPUT | INTERFACE
GUIDANCE
RADAR SELECT RADAR SELECT B RADAR SELECT A RADAR ACTIVITY
3200 Pes (44
BIT CODE
INTERROGATE PULSE
V2 GATESTROBE Y
FLATiSE ROTA =
112 + PITCH
508 2CMD TO DSKY 408 RR ENABLE AUTO TO OSKY 114 ISS TURN ON DELAYTO PSA
343 V, GATE STROBE
DISPLAY DATA
317 GYRO ENABLE
INTERROGATE PULSE SWITCHPULSE
(3 TYP)
DATA PULSE
° +z axis FORWARD
IWS TRUMENTATION aimee syRo assy AUTO TRK v3 STROBE
eZ
BINARY
aye)
1os.REFERENCE Sac Ca MoT i
i 1SIN i 1
cos 1 sin cos
GIMBAL, SWITCHING SHAFT TRUNNION Looe READ CATR READ CNTR
Locic, LosieAR ENABLE ERROR CNTR
cpu ZERO SHAFT
ERROR CNTR LOGIC:
wG 06 0G GIMBAL DRIVE CMDS ERROR CNTR ERROR CNTR
LOGIC Losic
A686 MG
‘THRUSTER “ON" FAILURE
seT TCA FAILUREStONaLy RESET
RADAR DATA
28 voc, @
GASTA SEE DWG 10.4.1 LAT VEL
FROM AGS
STAB/CONT. DAC OUTPUTS
cMos
AGS
RNG/RNG RATE
ccults,
enc |”ascent vaLves ENGINE
STBY (P06) pesci
came, 2 TYPICAL,
AUTO TRK ENABLE RR CAUTION
DSKY BISTABLE RELAYS
R305
@ airs
LIGHT TEMP CAUTION LIGHT RESTART
LIGHT OPERATOR ERROR
FDA ML PNL 1 9M6 PNL 2
DSPTAG +11aeIeAL reacken reocram ut oe DSPTAB +10 vi vi vi DSPTAB +9 ” m2 DSPTAB +8
DSPTAB +7 DSPTAB +6 DSPTAB +5 OSPTAB +4 DSPTAB +3 OSPTAB +2 DSPTAB +1
+o
vm * now VL, V2 AND NI, w2 Vi v2 NIN2
Ri (4) R1D1-05
D1 D3faa ce) bs2 ba R2 (#) R2D1-D5 Dr 03Ira c=) 05 a ce) R301-D5. DL D3R329 02 03 ys]
PTA IMnIBiT
iss WARNING
THIS DRAWING DEPICTS FUNCTIONAL SYSTEM FLOW ONLY AND IS NOT TO BE USED AS A DETAILED SCHEMATIC.
L0G ROR SIGHS INDICATE MOTION OF DPS ae CAUTION ENGINE BELL.
RNOZ ROR HE LGC WARNING WILL BE RESET BY EITHER A RESTORATION OF CAUTION NORMAL VOLTAGE OR BY SELECTING AGS VIA SWITCH 956 PNL 1.
THE 1SS WARNING WILL BE RESET BY SELECTING AGS VIA SWITCH 956 PNL 1 250VAC 800 HZ FOR ALL DISPLAYS EXCEPT AS NOTED FOR CAUTION AND STATUS POWER
10 LGC 2 NATIONAL AERONAUTICS & SPACE ADMINISTRATION MANNED SPACECRAFT CENTER - HOUSTON, TEXAS.
LGC OUTPUT
CHLA BITS 7,8,9
HLA BITS 7,8,9
wna air io °
imu stoBy
my OPR LUNAR
AND INTERROGATE ‘MODULE
MODULE
XLUNAR
28V 3.2 KHZ POWER SUPPLYSEE OW10,7 3.2 KHZ
Y PIPA BINARY CURRENT.
X PIPA CALIBRATION MODULE AND OC DIFF AMP AND PVR
£773 +2avoc10) *Z? Fie 10.7
Y PIPA CALIBRATION ULMODULE ANDOC DIFF ‘AMP ANDPVR
‘ZPIPA CALIBRATION MODULE OC DIFF
TORQUE (H
Tora GEN
Tora GEN
27s 10.7
LO-LIMIT THERMOS TAT
PIPA "PY &"N" PULSES
800 ~5 PHASE 8
800 ~5% iy. PHASE A 74) operate6
STB acc |MEMB ye |ate
IMU OPR +¥28v06
800 -5%85) pansea ELS 1007
‘Zs 107
aa) 28, gooax £27
1 MODES 30
MODES 30
MODES 30
iss
W LM UNIVERSAL REVA
WHEN READ CTR IS WITHIN © 0.1 DEG HIGH SCHMITT STOPS, FINE TAKES OVER. Fy GETS wy WITHIN TWO BITS OF 8.
RR CDU DRIVE PULSES REPRESENT(1) RR
SHAFT AND TRUNNION DESIGNATE CMDS OR
(2) FORWARD AND LATERAL VELOCITY (IF
CH12B8 IS SET, DISPLAY INERTAL DATA)
ISS CDU DRIVE PULSES REPRESENT(1) COARSE ALIGN CMDS, (2) MODE 1 DAP ERRORS , (3) MODE 2 DAP ERRORS, OR (4) DAP BODY RATES
GIMBAL DRIVE RATEIS LIMITED TO EITHER 35.5°/SEC (READ CTR AT 800 KPPS)
PROVIDES A GROUND PATH TO THE COARSE ALIGN RELAYS AND INHIBITS THE ERROR COUNTER ENABLE DISCRETE
THE RR CDU FAIL CIRCUITRY IS IDENTICAL TO THE ISS CDU FAIL CIRCUITRY WITH THE EXCEPTION OF POWER INPUT AS SHOWN
THE MIDDLE GIMBAL (MG) CDU SHOWNIN THIS DRAWING IS REPRESENTATIVE OF THE INNER GIMBAL (iG), OUTER GIMBAL (0G) RENDEZVOUS RADAR SHAFT AND RENDEZVOUS RADAR TRUNNION CDU'S
NOTES
DETAIL SHEET 10.11 .2
Vv l uU T R Q | P [ ° N M | L Y K J l I l H G F l E l D l ¢ | B A ia DATE [APPROVAL
‘SHFT/TRUN A Cm 71-69 1G.MG,0G, 1x RsvR OUTPUTS AR SHFT,TRUN 1X RSVR OUTPUTS 450" ‘COMMENTS:
ass
Teer vZ ‘eis & Lonpee G0 UM GUIDANCE COMPUTER(LGC) INPUT REGISTER MEMORY PROG/ROUTINE 10.4 Il RGA PATE SOME
9 PROG/ROUTINE WEWORY OUTPUT REGISTER ThaLie SoU BONEBUCEES wu Siétene ae Gt 25sec > THa8ve aK iz GASTA
imu woos 0s cma sir 24 \acouoeve ruses || , Voc p Tae | = “+A, MG COU DRIVE PULSES & PuL11 __4cazo1 98 8
tw woome ate: omen Th, a GDU ORIVE PULSES S anwrene 033 oar asta FLRNTO1SPLAYS e ©) Dap sr/sec7 rr : >J ant | a 7 seer eT oe epee ieee) OT Lee ov
Ta 1 GASTA8 DRIVE PULSES a RSVR 30° a2 90° > 10.4.1 mu MoDING 0050 ona BIT 15 At 0G Cou OR = 3 TootTAL +4 voc "Za a V. PRL 982 ‘COR FDA
Oar ———_ TO FINE. 4st Ae! a5" LOGICcil oS ‘COR5 = ey (rT FeTaL arruve4180TRUN COU DRIVE PULSES = sirens 22.5" a2 22.5 Jaa vneias our put 11 foes C+ 1 2 S002 RADAR MODING 0053 cHig Bit 12 “AB, TRUN CDU DRIVE PULSES — rao yacest ag ae 18S COU DISTRIBUTION Zs !
: = L COARSE SMTCH CONTROL SIGNAL COARSE 29-245 1x RSVR ELECTRICAL ANGLES — 90" 5.6) oat 5.6" Vie an SUL uZ2 (sc) +14 voc 0034 pap 1
8 ‘Ady SHAFT COU DRIVE PULSES SWITCHING : 2 i COU DISTRIBUTION .Z2 107 20 vac leLosie ast 2.8 a2 2.8 zavat ATTITUDE MON aeRADAR MODING 0058 ewe arr 11 hy SHAFT COU DRIVE PULSES i 10.7 es po "SeniteR ——_ 2s rx sreco a ce Dr ' PRE suceens ae = aZs. (Gy vieiee i
<———} _nor To COARSE a2 7 107 10.7 | sé swrrcHes a2 a5 uo vay, ous | BRANT POSITION FOAL
+84 ne 1G-1X RSVR SIN @ CAGE SIG a <==] 2° aa a = T a> eine Pore sii + ' *MG 1X RSVR SIN CAGE SIG swireHNG — az !
a 5 a3 és | aii Pati 4¢897— 18 Aaort Be 2 *) ¥ 1G -4 80, 10M +—P ELECTRONICS ' Pu. 2 227 OVERFLOW (,08") 6 '——— . a 1 R73 ASSEMBLY .1G 1x SIN @ RSVROUTPUT (800 ~ > 235! = he i
eg : 2 c-ayg imo. |G +080 2 | \ Then7) a2 % 6 6 «72 t7 42° ovERFLOW i ae Veonseowe ——{ os Fs aE we-000, > PAE (a) are] run sisthaeet 2Z® cone a Se ny’ |fi READ COUNTER (16 STAGES?10.7 ESET ec+a00, [D> _ rca estb AwBIGUITY RESET 6 1Lxsine 2.2 aZe STAB / CONT 4
1G 1X COS @ RSVR OUTPUT (800~) A b> Eine ° v MG ~A ve (ROLL) Te CONTROL 10.1 ‘el =e orwano | X-PATR seas wneur uae veteeny, | T-POMTER SOARE a
82? PULSES oe L +—s,61h 1G 16x SIN @ RSVR OUTPUT{B00~) > acreunte cm w ATTITUDE ci a Velocry, | eucis 408133| SYN PULSE ae. Oea ERRORS \ xe Ai MuLr 3 sas wee “ nea gina 62 omy‘Zs te aie wh
1x COs @ = 005 9, 10,7 42 HI MULT oN?
. AE ~ © = s MIN Acaus-6IG 16X COS © RSVR OUTPUT (800~) > ag ane a2" PHL 1is2. LoMuLT
“ weve conse ennon toy) SCHMITT coaRse Tennary Leven (i! coanse seuect » maiLacie (6 ciwgAt PULSE Cwo IIT pace oni mee 6 i f anes oye ad *ZsAND wpe OU ZERO 51.2 KPPS 1038‘© RSVR OUTPUT (@00~) . iavens ep
(- eens A swirenes) 18 cDU ZERO @) - AGS LATERAL VELOCITY ass FOR DETAIL OF ORDEAL 2AATERAL : t sakes /@ r Metis ewan _scn226
= | % a7 i AgsRoLly (we) mas A ss 800~ + sooHz
7 Sat ° fe DRIVE operant ‘SINGLE PULSE SYNC4 aT oy E W772 (10 SUMMER FOR RATE LMITING) PuLses | UP/OOHOTLORIE we euabee Pansprrcl SE FOAL Oy E eo ! * A) AORN AGTNG 1x 605 meek 8 Vee Ale WATT * ToTAL arTiTuoe aA‘RSVR OUTPUT(800 ~ ¢ seuecteo (s) SELECTED eReon | ec Oe PITCH ATT PONS ROLUYAW 3
seunie JZ? cro COARSE ERROR DETECTOR) genetzy 04g ==8 8 Za (96) s14v00 ERROR Se ROLLA a = HC EQ FE) | Mocad on 55 VAS mC wenB75 18 : 3 ats & S
a MG 16x SIN © RSVR OUTPUT (600 . 5 AMBIGUITY peg PONS ATT ERRORS AR ANT ostTioN
Serwnr F ¢ Awaicurry ox2eag.eoe> siltcR 125*<0< 235 Mee ° 8.6.0) Lo
2° FINE SWITCH CONTROL SIGNALS DOWN GIMBAL PULSES J UP GIMBAL PULSES DAP RATES ATTITUDE MON i ’ z 2 s PGNS ‘
MG 16% COS @ RSVR OUTPUT (600 ~) i le (Yaw ERROR/ 1. _artivuoe earorL. sons snooven 4 > ©
0G 1X RSVR SIN 6 CAGE SIG > " ue 0 DAP RATES he \ |-——— g PULSESELECT—| i * (MG) ROLL ERROR/OAP RATES \ ous.
ie 0G 1X SIN g RSVR OUTPUT (800~) > AMGSINEPHASE RATE SELECT Dp= Dac XCq Ug py PAL2 9810 1 PNL2 PNL16 _4cBi26 SELECTION FINE FINE Lret,é,ana [ Up=Yac +EyO ® RADAR RATE ERROR MON
ERROR TERNARY 5 2120) be+ ag MODE SELscHuItT LEVEL) ‘ - Loc RADARv Pe HIGH = 54, 45) Ay (Up) UP POLARITY PULSE sew s V,vay ‘ Aig @~costo -») LADDER ait rinecanon [So aa HIGH TERNARY LEVEL F, (Og) OWN POLARITY PULSE PULSE SELECT LOaiC poShraeATiONDEES SCALING AU. use maa his t+—+| asig=w Mee, fueANDQUAD “n> eve, nN Gacy agX8 | ATTITUDE ERRORS 384 PULSES X 11" 42.2 eur "ogg
4 0G 1X COS y RSVR OUTPUT (B00 ~) JA ATTEINATOR ce U v eR EN Mica tt be DAP RATES= 384 PULSES X ,0273" =10.5'/SEC — PNL2 987
7
=
384 PULSE X .044" = 16.8* ~ '° { | ° \27s 4 ' 1Z i | UGH OSPLAYS
ERROR CNTR e '10.12 0G 16x SiN y RSVR OUTPUT (800 ~) MG COS PHASE D/A POLARITY UP/ON Loic. Loc, Ags Loc i SHI AnaATTENUATION +947 Upp bursts bp, (Ou 2OWM Losic, Pe SLEW e RNOZ RADAR RR AZ/EL ANT RATES ROR RR ANT RATES ies X-PNTRsycos 8 Foy + ) 48 ane on Ye FORD us uP Locie sae SHATT/TRUNDESIGNATE auto Teac a oy =
Pogp)*Fon Dp DETECT SeerouEanon Pa 33 1 a | NEUee POLARITY DAG OUTPUT= .0132V/PULSE PGNS FORWARD VELOCITY ¥ 1 oxsowe |
90" PHASE ‘SWITCH 9K348 { i X-POINTER SCALE PNL16 4CB134 2av SHIFTER his Bo.”9298 FORWARD VELOCITY be ai800~1% t a PGNS LATERAL VELOCITY iv 1
a > 9x348 \y Te06 16x COS » RSVR OUTPUT (600 > ‘Zr ° min é 1—+ a + %e OL” 9298 LATERAL vetocity ie a MULT Ne 107 GENERATOR i 2 ——> el ee = ae R AGS LATERAL VELOCITY aie !: Ano iss ERROR Peru, +20, ' Lo MULTPs avaisoo-)A > en ya AhoyTan FRcTIONAL ay 2 counter TEM 16.875") SFrayo RUN ao iUNCTIONAL,
CAGE OVERRIDE CMD Bus S GENERATOR [——— ssi, AREAS ZERO z o " DEMODULATOR Ss im ' HL MULT27> SET 16x sin, cos aZ z +r B 4 oe Li LATERAL VELOCITY 7K298 Ev ", seweoe > J—» = : |r isl, berecr = oe pater [7 Zs Lanowws te ® pag SH [—s 2 “4 z VELORITY moe LR FORWARD VELOCITY ‘wom
RENDEZVOUS TRUN 1x SIN, cos 31.2 ee os se +26¥be 10:7 we “od SH98 Lomutt pac 2 Feas00sRADAR. RSVR (B00 ~), oZs pps ef, 2 —P +28.vor r Ls ane etsy — ERATOR |e oa .UM GUIDANCE COMPUTER (LGC) aso see €7' > O97 || : seaiees 25.6K005 Z a 28 — Lapoer xZe (2) nnTRUN 16x SIN, cos aii 5 -— F zy . Two
PROG/ROUTINE MEMORY OUTPUT REGISTER RSVR (800 ~) b> Jeuee HZ. GENERATOR War I |_# 2 70 NETWORK 10.7 nea VT 107 = 3 é -.
ze z = = GIMBAL Lock@ 2? Z Lid nZi DISPLAY INTERTIAL DATA TEMP OUT LIMIT +
7 cur2 5.60 107 B comere TRACKERISS ENABLE ERROR COUNTER ~<—f 15S ENABLE ERROR COUNTER (EEC) i ISS ENABLE ERROR CNTR (ED aiuke euasaatnee 2 avec ce IMU MODE cHi2 BIT 6 BUF ISSEEC ¢, # 11.25" COARSE [> we coarse auion
Le t LSE ff vZotee ERROR TO PSA ig 4 (cq) COARSE ALIGN ENABLEISS COARSE ALIGN ENABLE > ISS COARSE ALIGN ENABLE (CA) — n SUMMER >|TMU MODE cmizerr4 Bur WS, % FINE ERROR Bice INPUT REGISTER MEMORY PROG/ROUTINE MEMORY OUTPUT REGISTER5 +> > cmBaL LockSe = 1-4 RUPT DsPiiair 6 cH10
MG COARSE ERROR DETECT WGUPLINE COUNTER 1S WARNINCtmREAD FINB ERROR sheer ripnrte oS FREQ>160 GPS cH30 BIT 6 1-4 RUPT ss cou zeRo <4 18S CouZERO (2) ‘cou ZERO - IG CONRSEERRDET no ATTITUDE,
]
GE AR INNIBIT READ COUNTER Y) f Meeaoe 1-4 RUPT cHBIT §
18S COU FAIL ‘case cH30 air 12 1 MODE 30 1-4 RUPT cHaT a as wot _ AR ENABLE ERROR COUNTER ~<—f AR ENABLE ERROR COUNTER (RR EEC! AR ENABLE ERROR CNTR (©) “7sTa wODE ar +> 2? PROVIDES A CHECK OF 800 HZ EXCITATION AND INPUT CIRCUITRY aeELITR el “sven
; (by) 67.8" ORC =) Beare oy 16 C05 (6-9) ET —PY SCHPLME COUNTER ph BECOUPAI (cH30_ eit 7 RAD MODE 1-4 RUT osP 11 ait cH 10
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