I ~ I I IIIRCRA~ l Fil l No TIT I.I'" I , ~~l u N C tCONIIJENJiil-E V \ A V RO!:. C ANAD A LIMITED ••:. ONT A.HI/,) TECHNICAL DEPARTMENT (Aircraft) j -------- - - Arrow I ;. f- P()fX r N GENERAL I NTRODUCTION TO THE ARROW FUG.,T SI MULATOR PREPl\!1EO P.) DA rF May 1958 CHEC KLO BY 01\TE SlJPERVISF.C1 r,y DATE: ~.~~ 1 / ,t/1 ·///,'l/1 1 /1 1/ 11/ll/J RCPORT No ___________ _ TECHNICAL DEPARTMENT ------ - T-- AIRCRAFr I The Arrow Fl Simulator - i ght L-- SHEET N O 1 PREPARED B Y D AT E D . .J . t-~~- F~ \; '6 • C ht ECKED BY DATE UN & ~Wi=FIE D INTRODUCTION The Arrow Flight Simulator has been designed to provide a replica of the aircraft'~ pP.rformance oYer the range of flight conditions between t ake off and Mech 2.5 and up to altitudee of 80,000 1 • All known aignificant cross-cou~ling effects have been included and the variation of aerodyno~ic derivatives ~ith Mach No ., Altitude and incidence have been allowed for. I~ conjunction with the coc~pit and control sys tem simulat ion, it c an be used f amili a.riz: e pi b ts with t he per'."ormance of the aircraft, especi nlly from the point of vi ew of instrument display-. Alternatively, it may be used in conjunction with 8 simul at ion of the r &,far system t.o i nves t igate fire control problems . Two ways in which t.he simul Htor ha~ alreudy been used were to check out the suitability of t he control i:;ystem for t he aircraft, by linking the co~puter to the B-1 rig, and to check the behaviour of the controls ~nd damping syst~m installed in t h~ f irst aircraft, by linking the eimul ator to the aircraft control eurfacee and proYiding en auxiliary instrument pHnel in~ide t he cockpit. II /If} 11/lrll II I II II/flt, R!:."ORT No _ __________ _ TECHNICAL DEPARTMENT I SHEET No --~ 2~ - - ------ ,-------- - -- AIRCRAFT ----------. 1 1 The Arrow F] i ght Simulator I I I EQUATI ONS OF MOTIO~ P R EPARED B Y C H EC KE D BY In t he course of simulation, the six equations of m~t ion are f ormulated, specifically the li ft, dr ag , s i deforce, rolling moment, y awing moment and pit.ching moment equ ations . Cf t.hese , t he first t wo equati ons ar e i n t.hf! 11ind axes syRt em, t1nd the r emai ni ng four in the body axes system. Once the lif t ~nd dr sg f 0r ce$ have been obtained, t hey are r esol ved into thei:- components i n the body 1.1xes s.rstem. This h !:!S be.:in do!le because , al thoui;.-h t he boc.ly axes system i s more suitabl e for eimul cti on, people in r ener al are mor e f ami l i e.r ~~th the concepts of li f t and drag than of normal for ce and anal force . and The p~inci pe.1 pr oble~ t o ~e ov0r come i n mechani zi ng t he force mo r,ient equ2tions was that some of t he aer odynamic derivatives wer e functions of three Tari ables :- Mach Number, Al titude l:lnd I ncidence , By examini ng t he var iati ons , i t weg concl uded that a.n accept able approximat ion would be to separ ate the vari abl es, and take sums and ~ultipl es of funct i ons of e , ch of t he three vari abl es . DA T E D A TE R:::?ORT N O _ _________ _ I t N /J II/,'{ II II I I I I// I I /I S HEET No 3 A I RCRAFT TECHNICAL DEPARTMENT ---- 1 ---~~--P _R_E_P_A_R_E_D_e_ v _ _ -+-_ _ D_A_T_E __ I i I LIFT COEFFICIENT The Arrow 1'"1ight Si mulator CL = C4'_E (cx-O(oE) + CL 66 E.6e where C1txE = C¾() -g ~i n 9 + I coe i + lli (,57.3)2 57.3 M M Sideelip ·~=~ 57.3 - r + .21..rj (-Y~) + g coe 9 ein ~ + ~ T 57.3 ~ Bill p" = Ixz (I" + .£.S2 ) + 21..:J 2.L Ix 57.3 Ix Yaw • 0 r ~ ill p + Ix - Ir 129. +.lla.J 2.:N Iz Iz Iz ~7.3 ll.- - m · ~ + 57, JeT + .2Ll • LM 57.3 Iy 57. 3 I1 I;y In t he ahov" equ at ions, ell angles and ane-ul a r r ates a re in degrees. AIRC RAFT ' . -.. Th - -~,, •I I II () ~ /N I /(,I I l / / 111/10 RC?ORT Ne• ____ _ _ _____ _ MA -v" O:\.TA~10 S HEET N o TECHNICAL DEPARTMENT PRE P AR E D B Y Arrow Simulator l.ultiplics t ion n .. r. Fast•"' C H EC KE D B Y Because of t : e nonlinear chara~te:r of the equations of moti on, particularly whim the sp~,.,d and altitude are vurisble, a large nurr.her of multiplicetione w· re required. These DATE DA TE multi plicationa were performed by usinp servos and ganged potentiometers. In general, the multiplications could be sepw-ated into two distinct types. (1) Th~ multiplication of t ;·;o quantities which occur"d !:IS voltages in ~~e corrputer . (2) The multiplication of two quantities, one of which occured as a voltage in the computer end the othl'lr was a function of a voltage in t~e co!llputer. For the first type,~ servo motor was driven by one variable such that its aP.gular rototion from a ret'erence position 1;ras proportional to the variable . By exciting one of the ganred potentiometers with the second variable and driving the wiper by the servo motor, a Yoltage was picked off which was proportional to the product of the two quantities. The second type of multiplication may be most easily seen if we rir st consider how th~ function of a veribble was generated. As before, the s~r· o motor was positioned such that its r otati on fDom eome reference position wae proportional to the ar plied variable. Rc.-c>ORT No ___________ _ •I I It (I I I II I II I I I I I I/// I /,J TECHNICAL DEPARTMENT ,,Ai TO"- 0'..,TAJ; C, SHEET N O 9 AI RCRAFT· PR EP A RE D BY DATE A!'"r o.v Simul at or Multiplication Feb._ 1 58 C HE CKED B Y DATE .-----------------------------~-----------~----,,--- - The wiper moved uround a potentiometer ae the servo motor r ot ated , but the potentiometer had thirtee'1 tap point.l!I , e l:lch of which wae taken to a printed circuit card. On thh cm-c1 were thr ee bar:!!, one carrying a pol!litive reference volt !!ge, one carryinp- the neg.:;tive of thi s reference volt /jge a:1d the third gr ounded . By connecting each of the thirteen t ~pe of the potentiometer to one of t he t hree bue bars through an appropri ate r esi stor a~ arbitrary funct ion of the variable drivitlf, t he servo motor could be ~~tained. The wiper would pick off the value of the function appropr i &te to the input vari able . I f the reference voltage were now r eplbced by~ eecond veri abl e , then the wiper would p i ck off a voltage pr oportional to the product of thj ,r eecond variable and t he func t ion of the vt.iriable driving t.he servo. REPORT N o __ 70/5 1M/ 14-. _ I I R II I I II ( II I I I I I I I I// II , M A l 7" \'-j Q•,. T ;;. SHEET N e __ I O _ _____ _ TECHNICAL DEPARTMENT --- PREPA.RED BY D ATE ~RCR,\;;.- 1 AAAo.J ~llllt.ld\ .-0><_ . I CHFCKED BY ' - -- --,c-1---------_..---,--- Card rivative o 1 No. Functio Mach 1 Follow-up 4 CL5 9 5 CL09r3 6 CD0 +CE2 7 C 8 C,E 9 .G 10 H 11 12 1n1 13 jCAfo 14 lcMof9 15-~(a.c-c.g)/c 16.~CMt,9 I 17-t.Moefio 18 1'q Scale Factor ,4 10/57,3 40/57 .3 40/57 .3 40/57 .3 20 2 40 -200 10,000 -0.2 20.2 50.5 5.05 -2.2 -8.8 J I I I l I 19 le~ 20- ~R -.1907M I l I l.907M/5l 21 22 23 24 25 0 6r I I -1.58 -1.58 .632 -3.95 -1.58 7,90 Input 1.0 -l00v 1.0 -2 (.x- ~ 0) 4 ,.0 +2 (o< - tX O) g1 4.0 +2be 11 4.0 -20e".g.3 10.0 +l00v 0. 5 50CL2 5 .o i 2.0 I 4.0 I 1 ! I i 5 .0 l , 4.0 I j 5 .o . ; I 0,4 1 ! 0.5 i ! 2.0 I I I l.O ' ( I 2.0 ! 1 1 ~o l i I 1.0 1 1.0 I I 1.0 1 ! i 1.0 1 I 50CL(+&-) l00v -l00v 20e' -20e 'g10 -apq/a0 po r~aofo 2~M2p/po 2~Afp/p 0 Stx~fip/57, 3Po -2~M2p/p 0 50(~,?p/57 • 3P0 Output 40M -20CL -20CL +40CL 40CL 200CD 200CD 200Cn 200Co 200Co 20f11 -p0 ~16pPtf -p0 q/16plf -p0 q/16pAf -p0 q/16pl.12 -p0 q/16pi q/10 q/10 Y/l0,000 -YV/10,000 -YV/10,000 ETL/4000g20 ETL/ 4000g20 Y/2000 I ... ,l t\ I I Card No 26 27-2 '-~ ,:-,/h~- • ~,.':... 11 1' II I I It I II I I I I I . ! I l I , I ... f, "ORT Nt 7 o/ ~- I "'ii I 4- <...HEt. r "'<' _ 11 -·--- TECHNICAL o~eARJt'!'f_ENT _..J - ~ •H <> A FH- 0 8 v=._ _ 1-~ A T_F: __ , Dets ils of Mach a11d r-- D. J. Easter --1- ,April ' .SS - Al ti tude F\mctio!1 card s L-~ ~ H i:: c. " E O 1:1 v -+ o A TE Derivative Scale Load Input Output of Function Factor- Res istQt CY6rf19 7.90 1.0 -2ori2p.g12I P0 Y/2000 C~R 18.0 1.8 2plif2p/po r/10 I 28-1 C"o(p 2.00 0.5 -5o,:pM2p/57. 3P0 r/10 I ' I I 29-2 CI16r 30-0 Cn6ro( 31 f22 32 CnoaR macn 33 Follow-up 34 CnoR .f26 47 I Ch0 E 1,8 , .ChoE 49 ChcxE 50 Ch0 A I t f -1.080 I i i -1.080 ; , 12 .990 1 J -25.98 i l -64 .95 l t 10 .794 I l 2.0 5.0 1.0 5.0 l.Or/11 2.0 I 1.0 5 .o f r 5 .o 1 l I 0 .5 i 0.2 r I ' 5 .o '. ' i 5 .o ; t ! 0. 5 ! /_. . o t I I 0 -4 1 0.4 I s.o 0.2 -26r 9fi p/p0 r/10 -26rt#p/p0 -57. 3; /20o<. -2brAtpg22/p0 6r ' ':l'p/p 0 -26a 9 ti-p/p ,... r/10 -l0Ov 40M -26 1 Ai2J:. 57. Jr" /4<.lO p -20 Ag~3'#-p/p0 j -1/26 Ag23- ,23M2p/p0 -ar/abf°•r r/10 ap/ 80 ( 0 .P/4(+&- 1 ;;10 -2~M2p/po - 0(. ~ ri2/ 57.3 p Po 2orll2p/p0 -2or.l-p/pog24 -26 A tip/po 3 E.T.L. /10 p/40 p/4fJ p/40 p/40 p/40 r/10 -ar/ aopo ·z p/ 4J) 8(/aopo . p/4g26 P/40 -l00v -Hi/2 ,000 I 0.5 I 2 ~ 1-HF)'2,ooo 1 -H_g/2 , 000 I -4iAPort/l , 000 , 2.5 f -l00v I l I I I I I t-- ~ I I It , 1 I I II f II I I I I I 11 //I /~ .... ) . , ... REIOR' •. 70/ S.1 v J/1-'f- __ SHEfl , ; I 2- i A IRCl>,UT TECHNICAL DEPARTMENT , - - J - -- - - - Det .. ils of Mach and 1 - 0~ n ~: ~:~:ers ~ - _hnr: T : ·58 I Arrow Sim•tlator ... ~ - - t1 B.., 1. !\ T t- I Card Derivative No or Functfo l. I 51 ChaA 52 CtJo:A I l I 53 c~ ' I 54 OhoR ! l I / I 55 M l l 56 l M ' j 57 f(M)/J .P) l 58 I O(o i l I 59 o( f2 i ' I 60 I CM 08 2 I I l 61 ChoA i I I 62 Che< I I 63-1 t CYo(~ I 64 titude 65 Follow-up j I 66 gl I J ' 67 g3 l 68 g9 69 glO 70 g19 71 g20 72 g22 I 73 g23 74 g24 ·, 75 g26 Alti tUde Function Ca.rds 1 _ _ ____ ------[ Scale Factor -21.588 -21.508 93.78 93.78 0.4 0.4 1/4,000 0.2 0.4 .00630 -43.176 -35 ~866 I -72.6 I 1/so,000 1 1 1 1 1 l J 1 l 1 1 1 ) f Load Input Output Resisto1 0 .1 -20 A -HA/1,000 0.1 2~- - HA/1,000 0.2 2~Afp/Po HR/500 0.1 - 2oRM2p/Po HR/500 1.0 20M sl 1.0 8if" 3.2M3 1.0 I 40i?,p /P qc/100 10.0 100v (+~-) 20(0 ' 10.0 -50g2 2Lxo -40c2/50 1/16 q' £o 2.0 '-ic p 5.0 i -lOOv -HA/1,000 C1.25j -57.3p/v -HA/1,000 2 -FY/10,000 2.0 ~M 12 . 57.3 p 0 1 .oM f -1oov f ·, 1.0 r -2 (O'- - v( 0) ~ -2 Gx_-.l(,._o} gl 1.0 -lOOv I 1.0 ,I. 20e" 1.0 I K1ctto8+K2CM082 ! LO 28r M2P/P I 0 I I i 1.0 I rq3. TE ----------.._~ ....,_ ._.....,.,_,.......__ ------------ I ~ _70/_s1m ./l4_ . ___ I AVRO ,·l I 1-l C N , 1 FI /. IMI T/.: IJ !"'I E POh r 1-iO . ~ " ' TECHNI CAL DEPT l A •R FR A MEJ sn£l!T . . 2~1 --- -- - AIRCRAFT Arrow Simulator DATE . . Feb. '.5-.a_ -- --- -- WEIGHT . _15,000 . ..lh. -------- c. G . POSITION . 11290 ___ --· - PREPARED BY· _D. J, Foster. 1 2 3 4 5 6 7 e 9 Card No. 1 2 '3 J.. 'i 6 7 A Q function FollowuJ li-4i(R li~R[l vLOeR c1r, 0 r3 (;LJO+qEe. C C X E G. ~ . . () ? J, (1 n '7'7~ 0 . ()()Q m '- _,,,,_., -.oosa6 .j""°a3s I .5 2.54 .060 .773 .,052,__ __ &Q9.075 n ?./.? ~::: 6 t:::: i o? 2.73 .168 .773 .135 .00925 .. 325 .9 3.05 .418 .848 .385 00091.!J .. 120 =&l.Q __ ""~0029~ ... 1 110 3~27 .,74/J • 756 0490 .01680 ,,310 -.0156 .-.0022_,2_ I I I 1.05 3.18 .847 .670 .. 490 .0200 .305 - .0116 ,-.0020 1.10 3.27 .985 .659 .570 00221 .285 I r•.,00~6 -.,00238 1.15 Joa3 1.126 .596 0565 .0226 0280 -.0016 •.00175 l.W Jol 6 1.160 .476 .465 .0230 .25 ·-.0008 l .00172 -I 1.40 2.71., 1.082 . 304 . 335 00233 .,380 ... . 0050 .-.0013 1.70 2.lh 1.108 .172 .?? O ft n ?? ?. -ion '.,nn? ,- nm f.. 2.00 2.03 1 . 025 .138 .195 .0231 .475 :-.0018 i-.00125 2 .. 50 l.37 .780 .120 .195 .0231 .475 I I - .0018 i- .om ?'i ------------~ ~ ...... ¥ "'»~------------- . ------- i ~~~ . I ~~~ ; H RO A /R{. ?E-,J.f.. I o 8 9 17 t-----· ""-a; _ --fLlo• n~nn.l,Lni.;1.1 '11 ,._i::4-- --i=-:.-.....;2n~--1-•1LJ-· MIJ,.t.2JOA..i__~"'.c •. n~n1n~R..z..µ1•1..1a1· n~~:19..L_p 21L 6 - • oo 56 -L 25 I I ,0000175 -2.0 .0120 -.002 .08191 :.- . ,0l.7 -.0169 -1,~ .9 i-0000525 -1 .93 .0174 -.006 .0970 - .4255 -.0561 -2»95 1.0 i.0000755 -1.79 .0248 - .0109 .1266 - .4241 -.0735 -2.25 1.05 i.0000690 -1.70 .0264 -.0117 .1515 -.!.Oln - .0791 -1.00 I t--~•1 :..,,10 i.0000610 -J .61 ·-.,f)27L.. - .m 11. .159 5 -~ '½29 - .nRnn -'l :;>,; lol5 ,0000627 -1.57 .0246 -.0107 .175 ~.3113 - ,0729 -2.57 t--- --+---~---4-__;;___+----+---..;....+:-------+-------t------1~---t 1 .20 .000058 --- -1.54 .0219 - .0107 .179 2 o00 .nnno390 ____ ➔--=·2u~-..nf-. _, \,0086 .. .... ..,0073 .,J.62 2o50 .0000 390 -1.08 I I JI --,----------•--P._..,_...'l;"i_.,,..., ........ ..._ _______________ _ ~~ AVRO A lllCRA 1-·r L /,1/llt:O I f.L -OEP-;". (AIRFR AMl::.1 I SHE£T . . _-2,J. _ _____ .. AIRCRAFT . __ __Arr_(IJI.._Si!llll.1 at~- DATE . .l.eb. • . .!.58- . - . I . WEIGHT . . 55 ,OOQ Jh .. _ __ ' C . G. POSITION · - ---~ - -- .. ·- --- P REPARED BY . -·--· lL~ _;r_. _FQ~ter. I 1 2 3 4 5 6 7 a g -I - c .. ,.rt Ne. 19 20 21 22 23 24 25 2h I Cl.k CY~R CY~RV CY~v f21 CY6r CY5rf19 DeriTative f20 funr,t.-i on ~ M M.CM~ 0 .17 - _?. I. I , q -.220 0 0 0 .092 0 . 'i 1Q -.1'il8 -.245 0 -.00'5 0 .oq2 .ooq2 ' .7 .21... - . 1716 -.292 .225 -.017 .012 _no? n,q i I .9 JI. - 1.nSl'i - - 10'5 .225 -.0"'.\2 ()1Sl _og6 .o-=11 , 1 1.0 .77 -.1.?J.I-. - . '21 () () "' ()/.0 () nac; n":20 1.05 1.25 - ,1.2.lh -.117 • 075 -.rlhR .027 .oso .0L...'i • 1.10 1 .49 -.1.J.l.1 -.'2?6 ??Ii __ ogg .088 _mq .nl-.'i • ► 1.15 1.27 - .. 4206 -.116 .uo -.109 . , ,._,:, .083 ""a ·--- 1.20 0.92 -.4401 --359 .7'50 -.118 .201 .081 .070 . 1 .40 0.19 -.1..-=112 -.,25 • 7c;() - .. 1/...7 _ '21 f.. "" '2 n'JSl 1.70 0.16 - ,., ?f'\ - ')Jf.,. 1 .. 71 - 11f"I . ')')') ,oq6 .081 2.00 0.16 -.3759 -.220 .440 -.122 .2~ _()t:;f... _f'II:,? 2.50 0.16 -.3300 -.180 .2:,8 -.190 . ?l:.J . J 'l?O ()'lQ .. --....---,r-r - ~ n-.. ,. i, ,-.. ..... .. lk ,,,, I 1 I - 70/.Sim./ll_ --- l ;)JLP,{t_ ·l i ·11 (' ,,:,'/t(RAI /' / I U, / /; V I R- r'C; RT N O. I TECHNICAL o~_r_::FR~M£1 -7 S i'"' .. tc1T . . -~_,. 4.._ _____ D . .l . _ F2 atf}r AIR CRAFT . __ .Q.rr_o.Yl_Si rnulatQr_ DArE . - -- WEIGHT . 5 5 , QQ0 . .l.b .• - - I C. G POSIT ION -- .29Q - r •RE' f-ARED BY . - ·- - -- -' l 2 3 4 5 6 7 8 s -- Card No. 27 28 29 '30 'U '32 ~~~rr~~T8 C%R c°\3o<. Cnor Cnor°' f22 CnoaR I M - l 0 .02'58 4 - ,0657 -.nl1? .n?Ai=> n -.0111'1 Q5 .02690 -.0657 -.0413 .0316 .11 -~0110 . . • e7 . 027'38 -.1410 -.0419 .0'B0 .26 - .0110 .9 .02993 -.1770 - .0416 .0295 .4D -.0117 1.0 .04099 -.217.3 -.04D4 .0198 .52 - .0135 ~ 1.05 .05524 •.J071 ' -.0':198 . 021..0 .61 -.01?1 1.10 .04822 -.1963 - .0399 .0.300 .78 -.011 .3 1.15 .03366 -.219? -.0394 .0'328 1.00 -.0118 1.20 .03954 -.2268 -.0386 .0.319 1.05 -.0122 ·I f . 1.40 .03386 -.2346 -.0332 .0230 1.02 -.0071.. 1.70 .01614 -.3116 -.0226 .0256 -.0055 2.00 .01073 -.1156 -.0178 .0230 1.25 -.0050 2. 50 .00516 -.06'36 - .017'3 .0252 1.71 -.001..'3 , . l . I - .... ..,~~ I I -~ ~'~- /I 1 It o ·1 I I? i:· II ,4 I -, I I L'l / I f.1 I NEt" •• -;. C _70l SJm .['JJt._ ___ i HCHNOCA L OCPT. .10 .0108 '3 .01040 -.0825 18 . 336 • 0 /.0 'i - ?') 'l . 020 l _ .0126 1.15 .01139 .01287 -.0?55 17.865 - .J.J.'i -.218 .017 -.O'l1Fi 1.20 -01117 .m 1-:in -.0688 17.911.. -.L..00 - . ?()'i .O-:t? - . () ':tO 'i 1.40 . 00927 .01110 -. 0JJ,n 19 .Sll. - .'l"i2 -.228 . 042 -.0262 l . 1.70 .00735 . 00985 -.0340 18 .935 - . ,'50 - .27l. . 0 ':IP. -.n?m 2.00 .oo60l .00962 - .Q?6W 1 R . Q7 L.. - 'l 'iO - -:i?n .0?7 - n, 'i1 ' ' 2.50 . .00~'3 n nl-,/..o - n, -:ii:; 1 ll. 07/. - 1t:;() -. 172 ()1{-.. -.Olo11 ,. • .. .I _________ ._......,._r-_o,-c_,.......,.....,........._ .... ~ ...,,.. __________ _ _ ·-------! I ! I , 1 1, /lr; A/RcR ,11 I I. 1/I T/· /J ' I ' ! Arrow Simulator 7 ·70/Sim./14- __ _ . __ 2.7 ---- j AIRCRAFT Wf: IG HT C. G. POSITIO N Deri v ati Te ChO( 8 ) 1 Ch0 , 8 li'111'lt't.1 .. "' , M <""J AT E Feb . !58 _ .55,~QQ_lp. -- --·· .• ~90 _ ___ _ I PR E P.'\RED av _D. J. Faster t---~=-o - ~~-.&.·n.......,02>""'"-~ ~~ .... ~n1M..-'-01 _ +--.... -~0i012. -.001..9 .0025 -.0055 0 0 .5 -.007.2 -.0049 1.0025 - • 00 5 5 • 5 0 -·+--'·~•-,. 5_..._ 0 --t-- -- _ - - I r---'-· 7 ___ -+-- -· o_o_..13'-1-+~...,..=00=>2_ -+-_...;;•.;;.0_08::..;o;._' -1--..::•.;;.o..;;;..o...:58~ ..:.:• o~o;.;;;:2~5-~-. 0060 • 70 .9 -.0028 .. . oo, -.0099 -.0088 .0021..5 - .0075 .90 .70 ! I I 1.0 -.0030 ~.m2 -.0178 - .m 'il .00281.. -.0088 LOO LOO I t-----+...;...~;;...._~~:...__-+-~:=.4.ll::.._.~r.-'"'4,_.µ==--=1:..-.+- •= ~ -1-;;;._-~--- i 1.05 . 1.05 -.0120 .. 009 -.n?-:i.n -.fl1~2 .00431 I I -.0098 1.05 ·- 1.10 - .0130 . .. 024 -.0194 -.0156 .00$48 -.0104 1.10 1.10 , 1.15 -.0136 .035 -.0194 -.0215 .00536 -.0104 1.15 1.15 l 1.20 -.0128 ,. 01.R -.0185 -.02m .no6l8 -.0100 1.20 1.20 1.40 -.0134 ,.02? 1. /.{) 1.70 -.m -o mn - n,76 - .n?()}. .nm 'i? -.0160 , ?n 1 70 2.00 - .0124 .005 -.0151.. - m 6'i . 00277 -.0090 2.nn 2.00 2.50 - . 0116 ~.010 - .0132 - .0125 .nn-:i.~n - .nm'> ? i;n I I 1 1 -----------·-----------~---i.---··-------.;._--.....,.------' ~ • ia.:.• ,r;y,,~ .. , - ·. ' / "":-;;-)lk:;;;.,:r~ I I t-!FPC RT NO _70/si~-LlJ:. ___ ~~~- - a~ A t'R 0 ,, iR ( I< ~ F,r L I •I·.' I I i /.I T Z CHNICAL DEPT. AIRFR4MrJ Si-H: ET - - -2.8_ AIRCRAFT ____Arr.Qw.._ filmulator -- OAT'S Februa_!y _ _;L_.22!L_ WEIGHT . . 5.5 , Q00_--1. b • - ------- C . G. POSITION _ ·" 29.9__ _ ··-·- - PR F.: FARED BY . - D. J. Foate:r. _ , 1 2 3 4 5 6 7 8 9 . Card No. ,? 'iA e:,q 60 61 62 61 DerivatiYE tf' (M)p0 /t1 2 o< o o() Fl CARD Thrust Thrust Thrust ' 'hrust Thrust At. T I TV0"'" i () 1 ()() }.()() ] ()() 1?.9AA . 1712.5 25f.../ . 1 11R l/M. .nn1 . • R ( . .'V1J".' 5,000' .842 . 810 .871 l C.590. lll80. 15.l..O . 17 . 710. -1600. I 10,000' .?11 . 685 .770 8,180 6380 . 4560 . 17.150 . -10 ,280. 15 ,000 I . 599 . 608 .685 5,965. 8617.6 5593.1 16.848 . -19 ,251 . 20.000 1 . '50'5 • t; I.A .6oq '5120 . f-.?R() . 3.610 17 ')J,n - ?{-, Rf'\O - ?'i .000 I . 419 .477 ',/,/. J.£?'5 . 1 l.711 . 1 2ooq.1 ?/. ()') / . -'i'l.. ()1h ' 10,000' • 'J,}, J. . /.() 1 I.A? ..1.nnn 'l.,()t;(l '7ao._ ')') ?f"lt:: _,,, o0n , , 35.QQQ l .286 . 152 .l.20' 1'l..lh R 1sqs.1 - 'l.1.f"l.1 ?h n?A_._ l=i'7_,f)?f-. 40,ooo r .217 . 304 . '½l 2300. 2550 . 220 . 25.09l.. -,6 .'l..J.f... '50,000 9 .1575 .222 .257 - 200 'l..A/.n . 1 ()Q(). A172 .1 -1:; QA7 60,000 1 .1015 .167 .175 -711 .1 1,qn /, 1111. _q 7 'i'l..1 n ' -1 'l.f"l"7A ' 70 ,000~ .072 .112 .0'5'< -1.1.n .7 ?1 n7 1 f..Q() Q:; I /. 'l.., ~ , _..,,ni::.. Q 80,000 1 . 047 .057 0 - ?~? .• 5 l22R. 1 ln1.R I?/, 'l./, Q -1??'7 .,_ . . I I ___________ _.,...., ____ ~w.,..__ .. ~ ... •'t,.....__~J~ ·"'' .:~.:-:<:'I.lb-:::, _., :- ~ A// No , t In l N ,, 1- r l.: i,,•, ;- .- iJ ' : • I I ~., .. ..-- ,1~-- ·,o "'.. ~ .. ' ' ,.. I l t 70/Sim./14 ___ _ TECHNICAL DEPT. CAIRFRAMEJ 1.' I -------~ I SM~E1 , - i D~Tk ' _ 2, lJ, ___ ,__ ·- -- I AIRCRAFT WE IG HT C G . POSITION __Ar_:c_QvL.5.imulatDr ... -'-i' { -5..5 .,_000 lb . ____ :_ I• _ . 29.c_ __ _ __ \\ l.l, February 1~ PR!PPR ED sv. D. J . Foster : - ·- - -·- 8 -9 ~ 6 . 7 ~ Card No . iunc +. i on t) 8 1 g35 AB Thrust l1is.sm g36 A/B Thl-ust - 1n .11.0 a 1111.11h \nput p j input ~ input r ~ \ ·' 1 1-001 11-.00 ii.oo I I I \ I 5 ,ooo' ju,l.llO. I -u,29o! !1/J.022 j l.smi ;,_j .am I ,ru.u ___...1 __ _ l Q,0OO ' J 31 ,700. I -13,500: 1s.ooo' 13s,01s. I -14,7571 20,000, 142,069 . I -14 ,631J 25,000 1 J63,161. I -19~21] 10.000 1 112,142 . t -40_,132 35,r100 9 l56, 35s . 1 -15,1151 40 • ooo ~ • I 53,763. I - 11.i. , 3 3~ _2Q_7Q00 1 _J 18,294 . j -5242 . 20,000 2 J 12,040 •_L -3158 10,_oo() i _ l 6901.s I -1~10 .~ \! JI ao,000 1 3J~2J-~ ' _.-J029 ~E j' I 1/ 1077 l /1057 1 / 1037_ .1 1/ 1017 I 1 /995 1/972 ! lL9'Z.2__L 1/972 ,/ l ?T f \ 1/972 1/LJ - - -- - ~ --- 1'1 ' (, 1/972 \ 1/972 U \ I ' - '-T ~ ./Ji H I ' \ '\ \ :·1 .7122 - ~ ~- .7122 I \ I 1\ I ! -5921 .59~1 I -5957 > i , I _1.,_qis2 I ./.9.52 I _1,._q,:;-;, ,!&81 I . 49s1 t .4osJ.. \ I . 3'B6 J . 11':!h .11':IA l • 1l .?f:>65 .2665 I .2665 \ \ i.2] '21. ,?1 '.!L...~l....2111..... .1324 I .1324 J .1324 .oa19 l .oa19 1.oa19 ~05Q5-l_.o5.n5_ I oso'> ~ .Q'mO .0'¥>0 II"'.· ~~ ... . I t :;d&.,.'. ;_;,""' -'I V RO ·i I /I l /.' I / .' ! /::I , I l' I 1 0 . 7ol~L~Ll.4 __ • ~ - I I TECHNICAL OEF>T. CAlkC:RAMEJ SHC:".T . . _g_.12 __ - ·--------·- AIRCRAFT . ~w_Simul ator -- OAT£ - February_ 19 58 f WEIGHT --22 .000 lb.!- ----~ -- I C, G . POSITION _ .29g_ . .. . PREPARED SY . _o_._ J. -=~ate~--- 1 2 3 4 5 6 7 8 9 ·- - Card No. 89 ' 90 q1 q2 9, 94 95 96 Function a1/8 cf' ,af/acfo 3 2 p/Po ) ~ ' 1-'..,,_>I C!\11,'0 I Inout ~ Inn11tncn nt. l:i_ Eo Eo = -Rf E1 + ~ + + En En R1 ~ Rn E", :~{> Same n!I above 8.. Eo Eo = - (Hl E:i_ + N2E2 + .. . . .. NnEn) E "' C Int~grating amplifier. Add3 together E, ~. eever al inputs ~nd i ntegr ~tes t hem w.r. to time E. 2. E o Eo =-J. ) E1 + ~+~ . dt C R1 R2 Rn E l"I £ I Same as above E ._ N Eo - Eo =) Nl Ei_ + N2E:2 + N3E3 • dt fu E , OK E o Potentiometer Eo = K,Ei 0 < Kvl\q0<-r- Di ode f'LA;-1 Cr;flTu ot::>e:-, tvc t:oR~ 'F .. -¾\/vVv"--- Re!i~tor I - T Ground I I .J - .J d, U) ('I) ..J ~ - . t. .,. !-1.l . . ., .; _:_Lt I I r-_i-'- - --l - s··, I ' .: : I , ·,-;-i:, .; . ·I " I I I I· I• I +- , I -::-1 ..J ..J J en If) C'J f ',' C-----t ..I • OISTR!8UTEO BY RAPID [3LU( PiltlNT lTC, • 1-f-'Mll TnN, OUT, c.,..L.,!. C-r-~ -~::~ -~-=-~ ; h-~--0· .. i - I . -~· ··• ·:=--~-.., ... - .:-c..:·._::,, ~·. ~ •· l-. ., ..... _ h: t=::: . ., ... _j '.J..JJ J _;_ • I·:.·. ".i - • _j 'T: ·- I' 1 1 ·- 1-- -- - - .._. - ... 1• · -=.: ·-·' .. - ~ t..,....; -,.• t·t ·- ·+-~ - ' •• I •. , -· 1--- --lr-7" T • - - ; __ _. I~~•-' f.-- ... - ..;......._ .. ,J ' 1-, .. - •I j i-:_ _: :-:_ ►• .. 1-- µ 1 ,-;- . ... l ·-=:-.r+i~i ··1 ... j. l J :_; . -- ..... ---- . . ~+--- ·- -- -,--..,., ~·---1--- --·-.-- -- ,. • .i. ' ·;.'-:-rh· . .: _-_ J_..t. .. : ..... , .--.:::i:. ··f . , I i I .. I. l, I i l . - :~fr::~~_·'-;-_· ~ :--: ;i I ----- - I ...:. -. : I I . i ' I T t t l . -- ·- - - :~~- .. .T - •·· a:;:. l. , . 1 1_ ' +- -... i. .: . . •· l. + ] . == ., I .J l. .l.. -- i i i I I . 1·- • . . L . - J...1---- ·- -J---,~ c.--.. ~- le- . I ·, • I .. 1 : - . 1 .. f · i - ~.- .. ~-. -: ~:~:: +,...:-_: ' "T - --- ~ J" r- ._.:.:.t .. ' --'·-+-· - • · - rrr.._ __ 4--i--- ! _ ~-: ~.:; 1 -__;_ - -:..i.+ +4,..-L . ;.-~ --;.:.:.:.. : :.: I 1 X • ·- 1--t.J.- ; I _J___ . __ ·1 I -, , -=-r -- : . ..:...:..: ..... ,~·-....... ~---l----..,_ _ _,__--'.....,_ __ c.,.. . .:: i~:i_:_ ,\ _f.:~} I •••• f.-~--~~ -1- .-_- f:: l 't --~ -::. _1 'i' I •• • - I I I . 4--- -IOq ~- -- 1 • l >.-..... ---+--....-1 • ..,,..._ .,.t::-... ;::::::~,_-:..,r __ 1------"---- --4-- - • -=, ~f . ! , 1 · \ I , _,_,__+--_-+-:--+I -~-- ,j -I' ---i -- i . 1-~ I "I ~ + ~r -~~ .--~~ ~ll . • I I I ·I ,; I ,-, 1- ~ ~ : T 'l •. • j ' - . l . • f ~ '. . t + ! ,. •· L~ I I - 1 :.....::< - + . ....::. I . ~ . . • T ; ' I . .,.!- t I --~ --:: :-:- I - --+--- +--+~-1- 1 - • 1 -l-"---1-'--· ·-- -'+ -· J.1+.:.-'--'-+ '--·1+-'--J---,-\ I'/) ' N\ (f.) I ~ ~K: /I I/RO A IRCR4Fl I IMITEO M A LTON • ONTA RIO TECHNICAL DEPARTMENT -- . . . · - - - - AIRCRAFT c- !() 5 ~a 1....L D A. l'-1 PE. R. 0 ~ $ N ~~ / \ +~ Q._ < v0 ~ t- t0 ll 7\ -~ I: -...l I LI J < t l 8 ,~ REPORT NO _ ______ _ _________ _ SHEET N O PREPAR E D B Y DATE I IY w • j .A !lc 30 /57 D ATE/ C H ECKED BY < ~ N + ~ · ~, ~-r I \ M Vi ~ t --!Q £ J _ .,,, ~ , ~ ~ ~ I d: I - 0 I . ~ /\ -:-? -:- I . I -~~ .:-? ~~' l;t l I~ I ,~ ~I J ~ N I N • t YAW RATE GYRO ( INCL.l,J f'IT10 r-l .3,. !:," Oow,J) - r • 9-98 -.-)::>/ 4 · 2.+e, ?Ji- : I 00 K11 A ~ r =- 10 K,?.. ~r "" ~ .. l ·O K1-;5 ~~ =- .lQ "'1~ ~°v 2...5 -100 A "rsyro E:, ~a.. - ~a. l a_s - . o, br c.o..tM A ND ~ ;_ L I M IT" 50°/Sec. --------- ----- - - - --- I . I •01 I. 2.. ~-69 &i- • 1.3 2. . I . · '376 • I • O c_b !:;l .5 -t-1 ,. + RUDDER. J AC.)(.. - 2.. &i-- R UO DEA. 5 uRi=-AC.E" ~ :u () () :u ► '1 - ::i Q U\ K .... ,,, (') ::c ::!: );. (') :i: ' l> ~ ~ ,- ... i::i C z :.. i C , ~ ,,, 0...., ~ ~ ~ ::c ,. - ll-,.. -I - ..... 3: C ,.., ~ ~ z ~ .... -t ' ~ ~ ~ r -I ;o J) a fJl ;:• () 1) :t :u m r m 0 m m --i :u () 1) z --i :,; a ► 0 z :u 0 m m 0 L 0 Ol ~ -< Ol -< ~ ::,, C (i' 0 0 ► (>) • ► --i 0 --i m m - (JI V\ I AIRCRAFT: EK AVR O / 1 IRCRr ll- 7 L/M/T/-0 MALTON • ONTARIO TECHNICAL DEPARTMENT C-105 PtT'CH DAMPE.R. Al ." --tl w. \.I'.) I t r- J i.n -.-· I \ - < I \ a "' CA N~ . / -{ - -~ -~ l/) __.,___ _.... ___ Lfl I 0 ('J 2 ~ ..:.. g • \ " . . J ~;--.. tr':'~ ~0"'3 '-G :f I ,J ..J !I ~ , ' ~ ~ I \ l J 9 2 V y :.2 ~ 4 II) l/l Rl? r-ORT NO -- SHEET No PREPARED B Y D AT E J) tJJ. 1/,~ -,. CHECKED BY DATE w \.,0 I ' tj ...-j t.u ijJ o~ ;LL ~ u ~ t -- t t ~ j IO UJ . l,() • L,O I - 0 (J, ~L !El I r: '\J cc C II.I Ill ~ vO IP IJl I ,. ~~. I I A> fJ •II /U II II I I I II I I /J TECH NICAL "D r°P A RT M [ N T I.-__ sH_E_ET_No __ -=...--:..--:..-_- _-_-~---_-------------_----:_ I AO RCR~T- _- , 0_5' ___ • 7 ~ '/ Mus , T~ __ R ___ __J~-'3~·'_· :.J-~'.t..R_E.1::tP±,-c.:.A 6 R""EldD= s..__v _ _ -1-,L..,.,..,=·-D/!....A..!.~: --1-. E:...._,.,::::.-....!6':!.._.,.. bT9 -UL l i ()Rt9 - 7JH) - !] C H EC KE D B Y D A TE + o - ~o ,J Rc.L "-Y 11 1 o r,,~ + °?,u V -o (7 J 32 ) • hr--N-,---------1>-,..◄~a-Pc. ~ ( L RZ. 1- 315 - K3) o- ~ N O To C - 10 5 . + \r'I () ~ ~ \4 ~ V C\J ~ r g, w I ;o I'll 0 m -< -f l ,,, (') :::c ' ·I z -(') i - ):i, ;>.: ,- ..;~ C ,l_ i. 0 ' >.: ,,, 0 " -0 z ~ :I> ... > ::0 ,. - -4 ~~ 3: C ,,, ::: z ' -f ' .... " ~ Ill ;o I :, l'l 1l I'll 0 -i ;o z -t 0 z 0 A IRC RAFT l,C. 7 b. 4- ~ A V R I) , I/ R C I? , I I' r I. I II I r I I.J MALTOr-. ONTARIO TECHNICAL DEPARTMENT GR..ov:Jo f<,Pi. 4~ . I _ .b. Z.o - ,... ( \ R EPORT NO ___________ _ S H EET NO PRE P ARED A B Y t) . J. ~ CHECKED B Y N.I. ·;tr t, + + MA1>4 V'i~l::t'l.. \..l (, \~T •S5+ N .I . I.,C.?.t 2.'h tl l J + - N~ W'lila.. L IG I-IT"'. D A TE D ATE I .c;, 2.c... •U-t- ., .. .,. r ... ,-'- ~ ::.1 : : : : ~:;: p.:·~ :~:-,+a-..:J.: .... ... . ... ·-·. _, 1. - .... - . . .,. __ .. __ .. ... .. -- i 1-•, •• , • · · -r· . .. , : '.:..!" ; : ! .. .! · . JI .. , .. , • : 1: :.; .. . if :_:: .. . ........... - •1- t- •·:--... t •• ...,_ - t- .... ~ • • • '• • - 1 • T l G 9· 12 • 10 X 10 TO THE l f INCH 1-'AOL IN CMIAO.\ ~ t- ... . .. ··:- ~ :: . -- : :: ! !" ... +: ~ J~ .... ~ • • • ' • • • t . • • -, '. ' • ·r '-f'" '1 • ,- .. r • t t ·•- - - • • ., . :~;,;;.~-a:: .,, . -- ' ' ,J,r ''! . ~~ $_.B ~ ::'. : 'J ••. 1...-: r .; .v -- ·. I;,(:: . . . . . ~ . ... • - t-- ·- •• • • -4. • -- ••• -, - . . . r- . . . . . . , . ... 1. A V ROL C.A NAOA LIMI I c.O RE.PORT N, _, -::.j_s ~ , /_1+ __ _ TECHNICAL DEPARTMENT (Aircraft) SHEFT NO _±_._2.. _ _:__ __ ----- - -- --,--- PREPARED BY DATE AIRCR .\FT Arrow Simulator Face of Servo Rack C H ECKED BY [ ,. I I I , A'llplifiRr 1 Input Grid Outpu -- t 11.mpli Input Gri d Outpu fier t s of 9 Term.nal Intercon nection -- -- c1::.bl es Control Light 0 0 0 0 0 ~ ' ____ l 000 000000 0 00 0 0 ' I __::;roo REAC ~ 00 o o ~amping Overload Position Indicator - -0 0 0 aiO t:miJ tmJ o o oo o o 0 0 0 C!iD G:J t::ID Power SuPPlY ooo - 00 0 0 0 oo- -:JQQt> O 0 . 0 0000 000 000 oc,o .. o oaoooo 000000 ._ 0 00000 000, 000 00000 - -oo 1---------------4----- - Mul ti nli er 1 I npu t s A, B, C Outputs t.B I lQ_ 100 100 Multiplier 2 I nputs t.., B, Outputs .@_, 100 C J:&_ 100 Reeves Interconnections P~t ch Panel for one Reeves Servo 0 . - I:!li:J ~Loa ding Turret s Tapned Pots For u I'# ' ~ I €; • 0 - -l - -~ ~-a:T ~ • C c ' - -. [ - -- -• ~ ®ct V r ~ • C - ~ I. n - i ~4) ~ c; : ~ ..:±: C ·:L y;;- ~-:f' • ,) l • .. le (I! ~P~?-1.~u , "' • l~ (;1 • ., ' • • • . . . . " "l'·• ( &9&& t 0 ~1t~ ,. " i:, '( !I • • ... o I •••• • 0 •••• ' € 0 . (:. • ' ., ® ~ " . , I • " ~ ► • • • ti) "l • t) t?) e ~ • (:, . (!, . . . l @ ~ G G· 1 • " • • ... e • • 0 .. : •: . : 'Jl\Jr-l --- Ass,,... . •I[:-.. , J f8654•-• FOR INTERNAL PURPOSES ONLY. THIS Pi:r, ·· ,.. '. • '.: i; '-~l!ST N01 RE T l\ ': ~-- t' '. . , u 1 1 h t. P LA ,,J 1 A V RO E C ANADA L IMITED ~A l\i r,...r:..Ru TECHNICAL DEPARTMENT (Aircraft) Arrow Simulator ~ >< (!) 0 c.:, a:i Function Cards Rack Front view of fu'1ction Card Rack REPORT No 7..q/Sim/J4 S HE ET No __ _ j,,u...._ _ _____ __ _ P R EPARED BY CHECKED BY r-------------t---- -- I I I , Ur I nt PLAi~T. ~ II II r, Ii II ( N II f ff 111 fl /) C: 0 0 C •n ::l +> c.... 0 0 ~ +> c 0 co c.:> Q) P. r-i 'O OM ,9 J.. J.. ... c., 0 Cl) tll "Cl ~ c.:> i:: 0 .,.. +> 0 C: ~ 70/Si ;n/14 .!ii: 0 Ill ~ 'O H ~ ~ c 0 •n +> 0 c i · '--< I 0 ~ I Q) OM l> H I :-0 ~ ~ c· ' z 0 )> (/) U) - - 7J Ill ) CJ ~ a--. rOR II I TH\S P \r s:S G L) .. <;T ~- T:·1s P ' BE TMl{r _,. Pu5ES ONLY ' ~!' 1 ST NOT 1 OF THE PLA.~T t:.. -- --------- 0 LV. T r----------- ' ' - ASS FI:: K .. • I :" \,, 11 I T H l S r 1 ) J I; 1 BE TAKEIJ Ou I Or fHE PLANT I 483-1.pdf 484-2.PDF 483-3.pdf

General Introduction to the Arrow Flight Simulator. Report 70/SIMUL/14

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AVRO Museum

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