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Set  the  SPAN  trimpot  in  the  AP-1  fully  clockwise,  then  rotate  the  TURN  CONTROL 
from stop to stop and note the maximum obtainable aileron deflection. Adjust the servo 
RANGE trimpot as necessary to obtain about 50 of full aileron deflection at the limits of 
TURN CONTROL rotation. 

SETTING SERVO OVERRIDE FORCF. 

The  servo  TORQUE  CONTROL  nut  (the  locknut  inside  the  servo  on  the  output  shaft) 
sets  the  override  force,  which  is  the  force  you  feel  at  the  stick  when  the  servo  clutch 
begins to slip. 

Set the TURN CONTROL to neutral and then push the stick hard enough to override the 
servo. Set the override force to a value that seems strong enough to give fairly good roll 
authority, but not so strong as to be difficult to override. In subsequent flight tests, work 
toward setting the servo slip clutch to the minimum torque necessary to give enough roll 
control to handle a reasonable amount of turbulence. 

If you tighten the clutch enough to exceed the 30 in-lbs maximum torque rating, you may 
hear  a  loud  clacking  sound  in  the  servo  and  the  servo  may  disengage.  This  clacking 
happens when the force pushing the gears apart exceed the solenoid's ability to hold the 
gear  train  engaged.  This  is  a  redundant  safety  feature-just  back  off  on  the  control  nut  a 
little and recycle the power switch to re-engage the servo. 

CONNECTIONS TO NAV RECEIVERS 

Fig.  3  shows  the  autopilot  interconnection  wiring  diagram.  As  stated  earlier,  the  power 
and  ground  conductors  should  be  #18  or  larger.  The  servo  signal  wire  and  push-to  talk 
switch wiring may be as fine as #24, or whatever heavier wire is convenient. 

Use the supplied braided shield twin lead for the LORAN signal; do not use foil shield. If 
you  need  extra,  call  Navaid  Devices.  Ground  the  shield  on  only  one  end  (Fig.  3  shows 
grounding at the AP-1 end). This shielded wiring is necessary only if you are connecting 
to a LORAN—it prevents the gyro motor from lowering the signal to noise ratio. 

When soldering the shield, be careful not to let the shield overheat the plastic and short to 
the conductor. If you separate enough braid so that it can be held by a pair of needle nose 
pliers  while  soldering,  the  heat  from  the  braid  will  be  soaked  up  by  the  pliers  without 
damaging the insulation. 

The diode installed in series with the push-to-talk line, together with the wire connected 
from the PTT switch to pin 7, are used to kill the signal to the servo while the PTT switch 
is  depressed.  This  prevents  the  servo  from  jumping  around  due  to  the  presence  of  high 
level  RFI  (radio  frequency  interference)  on  the  power  lines.  The  servo  stays  engaged 
during the voice transmission, but it does not move until normal operation is restored by 
releasing the mike button. 

Содержание AP-1

Страница 1: ...AP 1 AUTOPILOT W GPS COUPLER AND S 2 SERVO NAVAID DEVICES INC 641 North Market Street Chattanooga TN 37405 Phone 423 267 3311 FAX 423 756 6154...

Страница 2: ......

Страница 3: ...ther or not they have a working autopilot Should you ever change airplanes you may want to use the autopilot in the new aircraft This can be done but you may need to change it from 14 to 28 volt opera...

Страница 4: ...ero turn rate 3 RATE OF TURN INDICATOR Electronically lighted bars indicate the rate of turn The center reference bar stays lit Additional bars lit to either side of reference bar indicate turn rate V...

Страница 5: ...p to your tracking signal you can relax a bit Just monitor the flight and stay ahead of the airplane 4 TURN COORDINATOR MODE When you wish to fly without the automatic pilot throw the mode switch to t...

Страница 6: ...give a neutral at 90 degrees or 180 degrees from that as supplied by Navaid The servo crank arm is secured to a flange by four machine screws that can be removed for indexing the crank arm 90 degrees...

Страница 7: ...easy to find a suitable site for locating an S 2 crank arm servo The length of the pushrod and to some extent the angle it makes with the driven element are user selectable The rod end bearing allows...

Страница 8: ...ows The servo pushes or pulls on a saddle bracket mounted on an aileron control pushrod the attach point being offset maybe an inch from the centerline of the control pushrod If the two pushrods are n...

Страница 9: ...7 WIRING DIAGRAM FOR HAND HELD GPS AND AP 1 WITH GPS COUPLER WIRING DIAGRAM Fig 3...

Страница 10: ...voltage between pins 10 and 11 on the rear connector of the AP 1 to zero or as close to zero as you can get it the voltage may wander a few millivolts Make sure that your voltmeter digital preferred i...

Страница 11: ...ull speed one way to full speed the other way Find the other point which is not really a point but a very narrow range within which the motor can be made to a stop or run relatively slowly in opposite...

Страница 12: ...e jinked to a new neutral Choose the longest possible crank arm radius that accommodates a pushrod range of movement equal to or exceeding that required for full aileron travel Be sure that the rod en...

Страница 13: ...ol nut a little and recycle the power switch to re engage the servo CONNECTIONS TO NAV RECEIVERS Fig 3 shows the autopilot interconnection wiring diagram As stated earlier the power and ground conduct...

Страница 14: ...nted units have digital autopilot outputs that are not compatible with the analog varying dc voltage signal required by the Navaid autopilot If you have not yet bought your navigation equipment please...

Страница 15: ...slowly rotate the TURN CONTROL from stop to stop at a constant speed You will hear the servo pause as the knob passes through the dead zone If you do the same thing while you are flying the wings will...

Страница 16: ...own then increase it to the point where the stick becomes jittery again With your airplane operating at its usual cruise speed set the gain as high as possible without oscillation or jittery stick mov...

Страница 17: ...out when you switch to Track which will introduce a tracking error if the TURN control input is anything other than zero before switching Therefore always make sure that the TURN CONTROL is in the dea...

Страница 18: ...that usually occurs at low altitude over hilly terrain If the cruising altitude is 4 000 or more feet AGL the autopilot should track the VOR without much S tuming or scalloping back and forth across...

Страница 19: ...tions But he should at least understand that there is such a thing as too much autopilot control and that a fast response to a hard over failure can be dangerous If you prefer a fast response then you...

Страница 20: ...gain using half the previous correction Three or four successive approximations for RIGHT CAL ought to get the time fairly close to the desired 2 minutes for a right turn Repeat the procedure on stand...

Страница 21: ...ng itself indefinitely The pair of interconnected sticks acts like a pendulum or flywheel that wants to keep the system moving The trick is to leave the dead zone as narrow as possible and still get t...

Страница 22: ...itched into TRACK MODE Make sure you followed the correct trim procedure then let the airplane drifts out as much as 5 miles If the airplane turns to run a course parallel to that called for by the GP...

Страница 23: ...ul if the relatively high pressure air on the bottom surface of the ailerons is sufficient to blow the ailerons up and thereby take the slack out of the system If you are still building please take al...

Страница 24: ...on heavy ailerons or a heavy spring in the trim system check with us We will probably ask that the autopilot be returned for checkout If we find that the autopilot is functioning there probably is mor...

Страница 25: ...on See Fig 4 on page 9 Swap the motor wires at the motor Swap end connections at the servo FEEDBACK pot these wires are white with red tracer and white with black tracer INSTALLING THE BRIDLE CABLE Ad...

Страница 26: ...r is on the end of the output shaft See Fig 4 for help in locating the FEEDBACK pot SETTING THE OVERRIDE FORCE The servo Torque Control nut the locknut inside the servo on the output shaft sets the ov...

Страница 27: ...A 3...

Страница 28: ...meter reading 2 The cover must be on the AP 1 because the gyro is sensitive to light Set your voltmeter to its most sensitive DC scale Put the AP l s MODE SWITCH in the center position Put either volt...

Страница 29: ...itch to the left or right for second The LED will rapidly flash alternately green and yellow and then go off There should be 0 1 millivolts difference between pins 3 and 6 on the AP 1 connector If you...

Страница 30: ...he green LED is on and steady then switch the AP 1 to tracking mode Relax Heading Mode Make sure that your GPS receiver is receiving and decoding course information and that the NMEA output is enabled...

Страница 31: ...he switch to the Heading position to increase course width by a factor of two Push the switch to the Course position to decrease course width by a factor of two After each push the course green or hea...

Страница 32: ...gine is started Attach the positive B power lead from the AP 1 to your avionics master a separate switch and fuse or a breaker switch 2 In some servo installations the sheet metal screws that normally...

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