As I said earlier I intend to use the scale closed loop system for the aileron control and have been giving it some thought over the last few months; here are the results of my deliberations so far and any comments and / or suggestions will be gratefully received.
I can see 2 main areas of concern; firstly the servo will have to pull all 4 ailerons with their associated friction and aerodynamic forces. Even though I’ll be using 2 servos, one will have to pull all 4 ailerons to bank left and the other one will have to pull all 4 ailerons to bank right. Secondly the cables may jump off the pulleys if there is any slack in the system.
The first concern is easily, if not cheaply overcome. I will use “high torque” servos such as Futaba 3010 and a 6-volt battery pack; it’s the second concern that has been taxing the old grey matter!
In a perfect world both servos would move the same amount and there would be no slack, but in the real world, using the differential mix, the servos will have to be set such that the “pull” servo moves less that the “release” servo to ensure that they are not stalled by working against each other but this obviously introduces the “slack in the system” that I want to avoid.
Below is a sketch of the linkage I’ve designed which I hope will alleviate the problem, I will be making a test rig before I commit it to the model so please get your suggestions in quick before I start!
This is how I hope it will work.
To connect the aileron cables the spring is removed and both servo arms and rods moved out allowing plenty of slack to connect the “quick links”, the servos are then moved back to neutral to take up the slack and the spring replaced.
To bank to the left the right servo pulls the bottom right aileron down working against the aerodynamic force, which will keep the cable tensioned, the top aileron is pulled down by a cable between the right ailerons and similarly aerodynamic force will keep the cable tensioned. A cable, via control horns protruding from the upper surfaces, connects the 2 top ailerons so the left ailerons are pulled up and again aerodynamic force will keep the cables tensioned. The cable from the bottom left aileron to the left servo is where the problem arises, here the aerodynamic force, which up until now has taken up any slack, will actually transfer all the slack to this cable run. Added to this, as explained earlier, the left servo has “released” more cable that the right servo has pulled, but because the rod can slide through the servo arm connector the spring will now take up the slack keeping the cable itself tensioned into the pulley.
That’s the theory anyway!
I can see 2 main areas of concern; firstly the servo will have to pull all 4 ailerons with their associated friction and aerodynamic forces. Even though I’ll be using 2 servos, one will have to pull all 4 ailerons to bank left and the other one will have to pull all 4 ailerons to bank right. Secondly the cables may jump off the pulleys if there is any slack in the system.
The first concern is easily, if not cheaply overcome. I will use “high torque” servos such as Futaba 3010 and a 6-volt battery pack; it’s the second concern that has been taxing the old grey matter!
In a perfect world both servos would move the same amount and there would be no slack, but in the real world, using the differential mix, the servos will have to be set such that the “pull” servo moves less that the “release” servo to ensure that they are not stalled by working against each other but this obviously introduces the “slack in the system” that I want to avoid.
Below is a sketch of the linkage I’ve designed which I hope will alleviate the problem, I will be making a test rig before I commit it to the model so please get your suggestions in quick before I start!
This is how I hope it will work.
To connect the aileron cables the spring is removed and both servo arms and rods moved out allowing plenty of slack to connect the “quick links”, the servos are then moved back to neutral to take up the slack and the spring replaced.
To bank to the left the right servo pulls the bottom right aileron down working against the aerodynamic force, which will keep the cable tensioned, the top aileron is pulled down by a cable between the right ailerons and similarly aerodynamic force will keep the cable tensioned. A cable, via control horns protruding from the upper surfaces, connects the 2 top ailerons so the left ailerons are pulled up and again aerodynamic force will keep the cables tensioned. The cable from the bottom left aileron to the left servo is where the problem arises, here the aerodynamic force, which up until now has taken up any slack, will actually transfer all the slack to this cable run. Added to this, as explained earlier, the left servo has “released” more cable that the right servo has pulled, but because the rod can slide through the servo arm connector the spring will now take up the slack keeping the cable itself tensioned into the pulley.
That’s the theory anyway!
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