ONNNNNN\p NNNNNNNNNNNNNNNNNNNNNNNNNNNNNNONNNNNNNNNNNNNNNNNNNNNN4@`  @`! #@%`')+-/1 3@5`79;=?A C@E`GIKMOQ S@U`WY[]_a c@e`gikmo/@`  @`! #@%`')+-/1 3@5`79;=?A C@E`GIKMOQ S@U`WY[]_a c@e`gikmo/CART_UP3ADDENDUM Et DESKTOP INF  RC_AERO PRGPt UREAD_ME \t qRC_PARMS040 s$RC_PARMS030 5t$RC_PARMS999 cu$RC_PARMS888 tv$RC_PARMS100%w$RC_PARMS200x$RC_PARMS400u y$RC_PARMS300Yz$RC_PARMS401{$RC_PARMS201N|$RC_PARMS101D }$RC_PARMS500~$RC_PARMS402I$RC_PARMS000$ Cartridge Update 1.3 Addition to Manual The following improvements to the R/C AeroChopper software have not yet been incorporated into the manual ISSUE 1.0 to ISSUE 1.1 ADDITIONS NEW KEYBOARD FUNCTION "B" Idle Up Switch Enable Changes the right transmitter button into an idle up control. NEW HELICIPTER PARAMETER Idle Up Low Throttle (- to +100%) This parameter defines the amount of main rotor thrust at low throttle settings when in the idle up mode. Pushing the keyboard "space bar" puts the helicopter in the idle up mode. There is a second way to put the helicopter into the idle up mode. Push "B" to change the right transmitter button into an idle up control. Then pushing the right transmitter button will put the helicopter into the idle up mode. In this mode the rotor rpm is kept constant and the power control controls collective pitch. Therefore in this mode you will maintain pitch and roll control at low throttle (collective) settings. The amount of main main rotor thrust at the low throttle (collective) setting is adjustable from -100% to +100% using the "Idle Up Low Throttle" parameter on page 3 of the helicopter menus. For example if the "Idle Up Low Throttle" is set to -025, the main rotor thrust will vary from -25% of full thrust at the lowest setting to +100% at the highest setting when in the idle up mode. The negative thrust available and constant cyclic control will enable you to perform smoother aerobatic maneuvers. If the "Idle Up Low Throttle" is set to a large enough negative value, you will be able to fly and hover inverted at low throttle (collective) settings. To get out of the idle up mode either press the "space bar" or the right transmitter button a second time. TWO NEW AIRPLANE PARAMETERS (on page 3 of the miscellaneous menu) Yaw-Pitch Coupling (0-9999) This parameter defines how much the airplane will tend to pitch down when using the rudder to turn. Yaw-Roll Coupling (0-9999) This parameter defines how much the airplane will tend to roll when using the rudder to turn. ISSUE 1.1 to ISSUE 1.2 ADDITIONS DISPLAY "ALTITUDE BAR" Push keyboard "3" to turn on this feature. A bar will move up the left side of the screen as the altitude increases. The range of the altitude displayed is adjustable using the "Max Aatitude Display" parameter on page 4 of the Heli Menu. For example if set at "0500", the altitude bar will reach the top of the screen if the aircraft altitude is 500 feet or higher. Push "3" a second time to disable this feature. DISPLAY "COLOR WARNING" Push keyboard "4" to turn on this feature. The sky color will change to warn of an aircraft that is too low for its vertical down speed. The color will change first to blue then purple then orange and finally (just before imminent crash) red. The sensitivity of the color change is adjustable using the "Alt. Warning Sensitivity" parameter on page 4 of the Heli menu. For example if set at "0000", the warning will start very early, but if set to "9999" the warning will not start until the last second. Push "4" a second time to disable this feature. DISPLAY "TELESCOPIC VIEW" Push keyboard "H" to enable the right "transmitter" button. Now the right transmitter button will toggle the "Telescopic View" display. In the upper right corner of the screen is a fixed size and position aircraft image. This enables you to see the aircraft clearly even if it is far away. Push keyboard "F" to return the right "transmitter" button to its missle "Fire" function. NEW AIRPLANE PARAMETER (Page 5 of Heli Menu) Airplane C.G. Adjust (+999 to -999) Positive values will move the center of gravity back and cause the nose to tend to rise. Negative values move the C.G. forward and make the airplane nose heavy. ISSUE 1.2 to ISSUE 1.3 ADDITIONS SOLID GRAPHICS This feature only functions in MEDIUM RESOLUTION COLOR. - Additional Keyboard Key Functions "7" Change ground color ( 19 choices ) "8" Change aircraft color ( 24 choices ) "9" Change sky color ( 30 choices ) "S" Toggles between solid and the old wireframe (The jet is always wireframe) CONTROL MODE This is now a menu parameter on page 5 of the heli menu. It is initialized to two. It can be either 1, 2, or 3. Keyboard key "1" which used to switch between modes 1 and 2 no longer functions. AIRPLANE AND HELICOPTER STABILITY PARAMETERS Improved function of these parameters. TWO NEW HELICOPTER AUTOROTATION MODES Two new autorotation modes have been added. The parameter "Autorotation On" on page 4 of the helicopter menu can now be set to 3 and 4 in addition to the old 0, 1, or 2. Modes 3 and 4 are identical except for the tail rotor function. In mode 3 the helicopter has no tail rotor control while in mode 4 there is tail rotor control. In modes 3 and 4 enter the new autorotation mode by turning off the engine by pushing the left transmitter button. The autorotation characteristics are now influenced by 4 parameters - Rotor Mass - Autorotation Efficiency - High Blade Pitch - Low Blade Pitch You can autorotate either upright or inverted. Control the collective pitch with the throttle joystick control. The collective pitch can be controlled within a range set by thee two new blade pitch parameters described below. When autorotating upright, a negative pitch will increase the blade rpm at the expense of an increased rate of fall. When autorotating inverted, a positive pitch will increase the blade rpm at the expense of an increased rate of fall. When autorotating upright, a positive pitch will increase the lift at the expense of a decrease in rpm. When autorotating inverted, a positive pitch will increase lift at the expense of a decrease in rpm. Be sure to keep ypur blade rpm high enough for controlled, safe flight. TWO NEW HELICOPTER PARAMETERS (on page 5 of the heli menu) High Blade Pitch (0-15 deg) This parameter defines the maximum collective pitch when autorotating in autorotation mode 3 or 4 (Autorotation On = 3 or 4) after turning off engine by pushing left transmitter button. 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Aircraft Collision Aircraft Collision With Moving Target Close Call - Crash Near Camera Aircraft Hit Camera Push 'X' to Disable Camera Crash The main rotor has hit the ground The tail rotor has hit the ground At the time of impact : The groundspeed was mph The rate of decent was mph Push M (Menu) to return to menu Push RETURN to restart flightH MINOR DAMAGE MODERATE DAMAGE MAJOR DAMAGE TOTAL DESTRUCTION From Proximity To Missle ExplosionFrom Proximity To Bomb ExplosionYou Crashed Into The Missle TargetYou Forgot to Lower the Landing GearYou Were DESTROYED By Opponents Missle!!! Aircraft CollisionAircraft Collision With Moving TargetClose Call - Crash Near Camera Aircraft Hit Camera Push 'X' to Disable Camera CrashThe main rotor has hit the ground The tail rotor has hit the ground At the time of impact : The groundspeed was mph The rate of decent was mph Push M (Menu) to return to menu Push RETURN to restart flightH  m7jRm7R7 -7nNu0-7|g;|A *0-Fpf -Hj ;| *;|0-F4g4ACFv&<a "-H|j;| *F`0-6g.AC7~&<:a t"-4ĂXRA8j;| *`j-7}g6 m8b.AC &<:a 6"-HRA8j;| *`,0-7|f&0-6g AC7&<:a j;|A *0-gR - HjkB`j:2-|(jDAH큂4-”|jDB.Aj4|mj;|! *+mHA *4g  * Hj * m7f0-Ұ|fBmBm7|g;| D4E 0C5Q BQA>N>g0-+Zf0-+Xg R0< a\AC~GfI ,6,T HC|Zk6<Zj4BRB|o4<5B4f5|` 0H@B@䀁2)HABA䁃N5AE 0RRAC~Gf0 H@|k0<5@ 0- Dg5| 0-6g5|25|Bj 0H@j|kp22)HAj|kr3A@AHHАҨ !A -"-$-A@aE 0a`T0|n0*j |k|5@>*ND:>*N8>*GND0>*GN2NuAC RN|G RCBBm$N# Rm$A 0a`(m+jC dE0S@G2A"22A"2Q4SB0hf0(jB@^@<6(g<<x6( HCCC|;|<@:-m̚m$jBEHᅊHEBE䅊|'k:<'02<@N><-m¾|k~AGj~:ND1G>N| j>< 1G@g -7` -km@1|>1|p0C d$m @G74<iF|2k<<2|j<<_FEE44:C<)iF|2k<<2|j<ND4>N68:*<0HFH@A1@0H@00H@1@>-GSG8Q4i-fRGA dCD;|@N2;m7N?<?<NMX|g"?<?<NMX|Mg|mf ;|`aa3/hNBy/hB40-6g 0-8tfNDA 00|k *hkBm DBC0-`f69/fA,aB0- *gA*Ta.A*la$`gA*TaA*a`gA*TaA*a`gA*aR0< aVP`hgA+a`TgA+,a`@ gA+Aa`, gA+axA,an` g A+iaZBC0-`f69/fAC`A:C]E ,0мB@H@aF00@A0jpмB@H@a00@A0@b|Zk@|j A*a`.|j A*+a`|j A*Aa` A*TaC *4g A+ag A+atBC0-`f69/dAa^0-6g 0-8tfND0<aQ?<?<NMXO *Rm2-mj@|g?<?<NMX|Mg|mf;|`|Xg|xf;|Fp`| fBmNxA 0BBh1|Bm *;m P0-F4gF0-+(g ;m+<+FSm+FBm Bm40-|oUmNABm@Bm@Bm@Bm@BPBm7|Bm7HBm7DB7a((;|bBm+B0-g0-`fN`N0-gNBab0-+(fa'd+mI+mIBmBm^Bm\BmBmfBmBmBmpA~ A4 +@p+@t+@x+@+@+@;@;@;@2-/Bfb;|~Bm(A0@ 00@ 00@;m78C|A4N?<?<NMX`L Nu|dkHd4|0H@`4<H H@2H@H H@NuHANuwwggggWGGGGGG7'6EDCB2"6@ʼ<<|# #X#2*DT!F(L,fDɂ ##$HX!2<< +(P(2 JJx_8-2Ab|(ddnU#/KZ((HP*+(-(>(7u527=X 54V5d    (   D   $S U, =p    Sd= (  H e     SH3   O  , C4$ \L ( \ z t 3(, P   <    R $  t (  |\, C  8= , p=      0=        B@|   8  8 <CC74   g  (   =$=H H  4,=lh          $ , 4`   (5  S     L      C<   4S@    ( 8=   =   = < D 4S0      0     M  U 8   @ 48   4    3    =     'X hɝ ܻ    8  6Sfs ݽ  L(/  ,    @ 4Cl 8w     gy    x sG   <, 5  8      (F  T    l 4 ( S D0(     = XD   4 ,=(== 006 (4    \4H,    9     ,   P    <  ,   L@t       G6 =D  `  L    H        = @     ( S   (=4   >  M$ $  G4(3(  8   /X   Z w4  xt     p l C   $   F  X 4D(܈ ^T4   0 SD@8 v   0$  0p؜   P  $ 4 u  3$ T  t 35  ʀ8 3  |  C    Pf   LH <    0h      $     3t ,4 8 P < L  D$  8 8     D4     =   DT ݀    D  $C  C        u7    +136`     Yvg  sgtH  J        m  SfE <  l, =$ $=G A 0 @  ,   L  B 8=< =L, @   x    0 5 ,       p  0      37xH   L 0D   4 C  P   [    0        ,8  $ 4  < ,H     $      $ $  T   $    ` T        =   p V` H$          7  ,    /A  ,     t 30    Th `$  $$ S  4 ( P D hT `  :<    ( x/  $ `   ` 4  6 t7,(8(    0 l l3L,       <4SHEY"+R/C AEROCHOPPERY#!Radio Controlled Aircraft SimulatorY$)Copyright 1986-1991Y%!Ambrosia Microcomputer Products, IncY&)All Rights ReservedY+ SOLID GRAPHICS REQUIRE MEDIUM RESOLUTIONY/#Push 'RETURN' for SOLID GRAPHICSY3 Push 'Space Bar' for wireframe graphicsERROR IN TABLE OF FA ADDRESSES H The R/C AEROCHOPPER SYSTEM MUST BE INSTALLED IN YOUR ST TO RUN THIS PROGRAM WITH THE COMPUTER POWER OFF INSTALL R/C AEROCHOPPERmemory alloc failure in rccmem free failure RCCY$(Push Left Transmitter ButtonY%(For Winch LaunchY'(Push 'F1' To Disable WinchY%(Push 'F1' to Enable WinchY'(Push 'RETURN' to Enable EngineY&(Scoring Flight CompleteY((Push 'RETURN' to ContinuePPPP=8AD*Ft   ƽ    ɽ ˧ͽ ˽ ijxpT r.N x   A H?<NNT0fZMJa?<?<NMX|g?<?<NMX| g| g&`?</G pp"m+*BGgbAEM@@?$rN`@``@`S@)Q`S@BC)AHABHBABQ`>f +*UG+H<F7`RG|j"m+*<`j<F03` m+P"m+*$m+.&m+2(m+6QRE|k m+*+H+^"H'+H+b$H+H+f&H+KB+KE+KB +H+re+I+j+J+n m+^CzEH0<Q;|@aH;|'vA @ @ 0@;|, 4XmB;| <;| >A/+H @;| H+yMGN+|0<A,CE.GQ;|Z;|-;| ;||;|b;|;|;|+|+|;| ;|c;|L;|;|;|L@;|&;|;|F;|';|' ;|@L;|@X;|c$;|c$;|$I><?NN;@`tvJm`ftvAI0<2AagC8DD@Q0-`f;| ;|$bA@+H+H;|;|;|?+|'+|6';|';|';|@!;|!;|!+|!;|0;|L;|L;|\;|\;|];|?]`;|Ib;|\;|\;|0];|~]A+H+H;|;|?;|+| '+|l';|';|';|!;|(!;|!+|!;|p;|L;|L0-`|fn;|\;|\;|0];|~];|L;|;|';|';|$;|$+|!;|;|!;|;|PL;| L;|N';|' y m`g Apa6a N*NN@Nn m`f2AI0<2A8DD@QA0<24AP1QA |5N?<"NNT @C+I$+h m`fe3enG"6 m`f"666 6666 6` 66666666ApNl3enByeNv3neJm+(g ;|]Bm` m]f BmNj` NjB0-]F@;@]0-6g +|t \m0-`fSma*0-F4gBmABmF40<La60-bjD@@;@0-jD@;@I;|BmIB-IBmABm@Bm+"Bm@0-ܰ|f+"B@Bm@a Bm;|/@+m8j+m 6Bm+v;|B@BB+XBm *0-+(gFqa +Z`0<Da5p0-6g\mBm+aBmBm^Bm\BmBm0-g m`k;|Bm;||Bma jBmBm;|E#CCANP< gH4`AEG"6E#09E+I8dS@6<"X2)4|k6<@Â86)CCCSD7A62)f 4)SB2<`ȃ6)CC4iSB:-`|fAB7A7BPQA#BBB"B&Jm+(f0<La4F0<Ta4>a pa a -+Vfaa0-@>ND2>NHᇏA00-!@1@2-!h1A@1AN 0-@A0|(D@"<33A0N3LN78aAa3ne m`g ByeBynApJyeg yNlRL-LgNqa~0-6gRm70-7|k0<2a3:;|09090-+Vg@Jyef m`fe yNlBm+V0-g70<1a2`|0-+(gRm+F0-+Fm+N>MMPat0-6g 0-8tfND?<?<NMX|gBmABmFBmF4a0<La1 ` ;|;FSmF0-g0-6gj0<2a0`^0-Ұ|gV -H~@jJaA<N@0(hf\g AFj8B0-+(g m+$CXXXX+H+$0-faR0-bgBm@A4C|N-ACDN20-\g>0-4m]6-\Ĕm4-]>-\ mf ACZdN20-7g,NA;|( f( faaľaZ -GNGVfAMCF<cf0- *f 0-6gND-@fN m`g m]g - 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Go To ........ Misc Menu Airplane Menu Wind Menu Control Menu Heli Menu Main MenuY >R/C AEROCHOPPERY!4Radio Controlled Aircraft SimulatorY"*Copyright 1986-1990 Ambrosia Microcomputer Products, Inc Y#:All Rights ReservedY&,Parameter Set Up MenusY*,Store Parameters on DiskY-,Read Parameters from DiskY1,Flight DemoY4,Fly HelicopterY7,Fly AirplaneeY :PARAMETER MENU CONTROLY";Update ScenarioY&FUpdate Misc Flight Parameters Wind Parameters Helicopter Parameters Airplane Parameters Control Parameters Go To... Misc Menu Airplane Menu Wind Menu Control Menu Heli Menu Main MenuY (MISCELLANEOUS PARAMETERS 1 Sun Angle (5-90 deg)Time Adjustment (0-600) Missle Acceleration (0-1000)Missle Size (1-9999)Bomb Acceleration (0-1000) Bomb Size (1-9999)Field of View Horizontal (30-90)Field of View Vertical (20-60 deg)Y (MISCELLANEOUS PARAMETERS 2 Aircraft Size (500-2000) Rotational Size Change (4000-8000)Camera height (0-728 ft) Initial W-E Coord (-999 to +999)Initial N-S Coord (-999 to +999)Initial Yaw Orientation (0-360 deg)Restart wait time (0-9999) Winch Launch Direction (0-360 deg)Y (MISCELLANEOUS PARAMETERS 3 Yaw-Pitch Coupling (0-9999)Yaw-Roll Coupling (0-9999) Maximum Frame Timer Count (5-30)Missle Target Range (60-9999 ft)Glide Sound ( 0=>off 1=>on )Other Pilot Offset E-W (-to+ 999)Other Pilot Offset N-S (-to+ 999)Missle Hit Radius (5-500) Y (WIND PARAMETERS 1 Wind Base Speed (0-250) Wind Base Direction (0-360 deg)Wind Speed Change Freq (0-9999)Wind Speed Range (0-100) Wind Rate of Change (0-20) Wind Duration Max (0-100) Wind Duration Min (0-100) Thermal Base Speed (-100 to +100)Y (WIND PARAMETERS 2 Direction Change Frequency (0-9999)Direction Change Range (0-360 deg)Direction Ch Duration Max (0-100)Direction Ch Duration Min (0-100)Turbulence Frequency (0-9999)Turbulence Peak Vel Max (0-60)Turbulence Peak Vel Min (0-60)SpareY (WIND PARAMETERS 3 Gust Frequency (0-9999) Gust Peak Velocity Max (0-90)Gust Peak Velocity Min (0-90)Gust Direction Max (0-360 deg)Gust Direction Min (0-360 deg)Gust Duration Max (0-100) Gust Duration Min (0-100) SpareY (HELICOPTER PARAMETERS 1 Side Drag (0-9999)Top Drag (0-9999)Front Drag (0-9999)AA Lift (0-600)Translational Lift (0-300) Collective Lift % (0-100) RPM Lift % (0-100)RPM Slow From Tail Rotor (-to+300)Y (HELICOPTER PARMETERS 2 Yaw Engine Torque (-999 to +999)Yaw Relative Wind (0-1000) Pitch Relative Wind (0-6000)Yaw Spin (100-6000)Roll Spin (100-6000)Pitch Spin (100-6000)Roll With Vel (-999 to +999)Sound Adjust (500-2000) Y (HELICOPTER PARMETERS 3 Pitch Stability (-999 to +999)Roll Stability (-999 to +999)Weight (13-1900)Pitch Inerta (50-9999) Yaw Inerta (50-9999)Roll Inerta (50-9999)Ground Effect Amount (0-1000)Idle Up Low Throttle (-to+100%)Y (HELICOPTER PARAMETERS 4 Autorotation On (0 - 4) Autorotation Efficiency (30-1000)Autorotation Pitch Stab (0-9999)Rotor Mass (400-9999)Collective Lift (0-400) Image Number (0-2)Max Altitude Display (8-9999)Alt. Warning Sensitivity (0-9999)Y (HELICOPTER PARAMETERS 5 %Pitch at 50% Control (0-100)%Yaw at 50% Control (0-100)%Roll at 50% Control (0-100)%Power at 50% Control (0-100)Airplane C.G. Adjust (+999 to -999)Control Mode (1,2 or 3) High Blade Pitch (0-15 deg)Low Blade Pitch (-15 - 0 deg)Y (AIRPLANE PARAMETERS 1 Side Drag (0-9999)Top Drag (0-9999)Front Drag (0-9999)Yaw Relative Wind (0-1000) Yaw Spin (100-6000)Roll Spin (100-6000)Pitch Spin (100-6000)Pitch Relative Wind (300-6000)Y (AIRPLANE PARAMETERS 2 Pitch Stability (-999 to +999)Roll Stability (-999 to +999)Weight (13-1900)Pitch Inerta (50-9999) Yaw Inerta (50-9999)Roll Inerta (50-9999)Wing Asymmetry (0-3000) Fuselage Lift (0-70)Y (AIRPLANE PARAMETERS 3 Image Number (3-6)Coefficient of Lift (15-200)Start Stall (0-90 deg) Fully Stalled (0-90 deg) %Pitch at 50% Control (0-100)%Yaw at 50% Control (0-100)%Roll at 50% Control (0-100)%Power at 50% Control (0-100)Y (CONTROL PARAMETERS 1 Pitch Delay (0-31)Pitch Sensitivity (-125 to +125)Pitch Trim (-999 to +999) Pitch Rise Rate (0-9999) Pitch Instability Incre. (0-9999)Pitch Instability Max (0-9999)Pitch Instability Freq. (0-9999)Pitch Instability Duration (0-9999)Y (CONTROL PARAMETERS 2 Yaw Delay (0-31)Yaw Sensitivity (-125 to +125)Yaw Trim (-999 to +999) Yaw Rise Rate (0-9999) Yaw Instability Incre. (0-9999)Yaw Instability Max (0-9999)Yaw Instability Freq. (0-9999)Yaw Instability Duration (0-9999)Y (CONTROL PARAMETERS 3 Roll Delay (0-31)Roll Sensitivity (-125 to +125)Roll Trim (-999 to +999) Roll Rise Rate (0-9999) Roll Instability Incre. (0-9999)Roll Instability Max (0-9999)Roll Instability Freq. (0-9999)Roll Instability Duration (0-9999)Y (CONTROL PARAMETERS 4 Power Delay (0-31)Power Sensitivity (0-60) Power Trim (-999 to +999) Power Rise Rate (0-9999) Power Instability Incre. (0-9999)Power Instability Max (0-9999)Power Instability Freq. (0-9999)Power Instability Duration (0-9999) $>:^~\PEI\4$&0@H JȔnŊp$PȮĒd>bJn4,PĒʄ>b:.d ߌߦN%22fER2f]j}  ,;$`,;$=K$`=K$M[$`M[$]k$`]k $m| $`m|  : ::88*8.:8>J8NZ8^j8nz8~   .;N[fsJ~JJJ b&2<'46B<7DFR<GTVb<Wd fr <gt \ \\&p &p,&p,<&p<L&pL\&p\l&pl|&p|  <4TTTlJ=JMJ]JmJ}<\t5EUeu`$`$`$Y&GY*JY-JY1?Y4?Y7?Y#3Y#>Y'@Y'IY)@Y)IY+@Y+IY-@Y-IY/@Y/IY3>Y3cY5>Y5cY7>Y7cY#DY%DY'DY)DY+DY-DY/DY1DY3=Y5=Y7=Y'@Y+@Y.@Y17Y47Y77Y#1Y#8Y&;Y&BY(;Y(BY*;Y*BY,;Y,BY.;Y.BY3+Y3DY5+Y5DY7+Y7DY#DY%DY'DY)DY+DY-DY/DY1DY3;Y5;Y7; (                 f2 &7@(* +778~|+ zv x x"$&zI`x]]'.'0'2|ZD]hLhN"$&'.'0'2| 7`bdfhlx77 ,7F(L(GJ  F( Fn F(x KU;8F#qF(4(F( Z d ZF( FFL2F F (Z h  <  h   Z <   , d  Pd  P  X  F ( d@ dL  ,<(-#h2 F< , - 2hP22pp,, 5d(((K rTF22#,,^ 5d(((K `@mA22#  5d(((K@n<22 [d 5KKF222Xd 5###KF#722244KF 5(((KF#R222qRRKP 5222KF#R22ddq::}P,222K(,22 X^~~P(P 5###2(22 2^~~P(P 5###2,< X22  F"}(((K p' 5p ((72222   (,X#22x d ###2x  }F###2,@ T[@ x(((2xddqRRP<O2222,AdP0Z(((2XLAF:P---2d^f dMB#22222Fx d&!(<2222PXPP<(#2#2X @X   ,,,'''',''U- Next Page.... 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kknz`">-APk kk k^knV6+kC m B4jDBEn,$H(rj5ro5ЂXAAj`$REh$j4<`4<Hk>(rj5Ђ(ro5RDXAn޸rj58 ro5`n(ro5Ђ(rj5SDXAn޸ro54 rj5`0kDAArj5rj5ro5ro5Q>f46)C 02)~|`I$0+4vTjCDC8< m`f@8:-$kERC:-`|fmnx:+ E2,EjrL:-La-$f -$fdRAb@Ak>Lf fSBjBBH m"&mC630HGfOM0-"H26ZloT`ޒljrZlk̖lkv8<:<-AEA>-aHCEnn>-IfJ>FGf@DE|6SC2:f8-`fZDVD|fWD1@f(` f" EgTCf `EDFF>6`sPFGQQD`:E>3PFGQ!>FGSGk FDQ!QF>7`FGQQ.mr0-INu4@*" $ p D,     ~ vTJ T &V |,$ @ 02h $N(Z $X& Lp  d>Lp&:*RԂ        v      ̲ RNR>p$FF    $   v         8 ZpD@~"Rj 2 | Z$N..,,":B@84,(<\>T6 &X<@T&H (  P ~ 0"&"L"N$v^*TV 0Z ^ Z Z   *X <:&f  (hxdh&rp$:$8"  & <:,8"   <   H Ambrosia Microcomputer Products, Inc. 98 W. 63rd St. Suite 371 Willowbrook, IL 60514 R/C AEROCHOPPER UPDATE 3 DISK INFORMATION The RC_AERO.PRG on this disk can only be used by people who own an R/C AeroChopper system. With the R/C AeroChopper system installed on the Atari ST, run the disk based RC_AERO.PRG. This program enables the R/C AeroChopper system to use the Atari SM124 hi resolution monochrome monitor for display. This program also enables issue 1.0 and 1.1 cartridges to have the latest features. The Addendum to the manual on this disk (ADDENDUM) explains the features added from issue 1.0 to issue 1.1, the features added from issue 1.1 to issue 1.2, and the features added from issue 1.2 to issue 1.3. This program can be used with all R/C AeroChopper cartridge based systems. RC_AERO.PRG is copyrighted by Ambrosia Microcomputer Products, Inc. You are authorized to make backup copies of the R/C AeroChopper Update disk only for your oun personal use if you label the disk as follows: R/C AeroChopper Update 3 Backup Copyright 1986-1991 Ambrosia Microcomputer Products, Inc. All Rights Reserved  9999 9999 9999 9999 9999 9999 9999 9999 0030 0285 0007 1500 0007 0700 0070 0040 1000 6144 0005 0000 0040 0325 0000 0330 0000 0000 0011 1000 0001 0010 0020 0015 0015 0000 2000 0020 0007 0025 0025 0000 0010 0010 0010 0005 0500 0010 0010 0000 0000 0000 0000 0000 0000 0000 0000 0500 0070 0025 0300 0085 0050 0050 0050 0000 0070 0500 0500 2000 2000 0075 0500 0000 0000 0200 0250 0050 0250 0250 -100 0002 0190 2000 1950 0128 0000 0008 0000 0040 0040 0040 0075 0700 1400 0100 0100 0369 1618 1618 1500 0000 0000 0165 0286 0080 0286 0572 0007 0004 0079 0018 0030 0050 0050 0050 0050 0000 0030 0000 0000 0000 0000 0000 0000 0000 -020 0000 0000 0000 0000 0000 0000 0000 0030 0000 0000 0000 0000 0000 0000 0000 0015 0000 0000 0000 0000 0000 0000 ? 9999 9999 9999 9999 9999 9999 9999 9999 0030 0285 0007 1500 0007 0700 0070 0040 1000 6144 0005 0000 0040 0325 0000 0330 0000 0000 0011 1000 0001 0010 0020 0015 0015 0000 2000 0020 0007 0025 0025 0000 0010 0010 0010 0005 0500 0010 0010 0000 0000 0000 0000 0000 0000 0000 0000 0700 0070 0025 0400 0055 0050 0050 0050 0000 0050 0500 0500 2500 2500 0075 0500 0000 0000 0200 0250 0050 0250 0150 -100 0002 0190 2000 1950 0128 0000 0008 0000 0040 0040 0040 0075 0700 1400 0100 0100 0369 1618 1618 1500 0000 0000 0165 0286 0080 0286 0572 0007 0004 0079 0018 0030 0050 0050 0050 0050 0000 0030 0000 0000 0000 0000 0000 0000 0000 -020 0000 0000 0000 0000 0000 0000 0000 0030 0000 0000 0000 0000 0000 0000 0000 0015 0000 0000 0000 0000 0000 0000 ? 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