Wow, genuinely amazed at the response to this. Thanks to everyone for the replies and input. Plenty of interesting ideas floating around there.
To put things in context, this project is already far beyond what is needed for this thesis and although it sounds counterintuitive I need to try and keep the electronic controls as simple as possible. Reason been the course I am completing is mechanical engineering so too much focus cannot be placed on the electronics alone. In regards to having progressive control there's no real need for it. As under braking the wing needs to move as quickly as possible. And then back to high downforce once the braking is finished. Also, hydraulics cannot be used as its a safety issue. The forces involved at the high downforce levels will be about 1500 newtons. As for when the wing moves to air brake mode, as the wing is in stall this needs to be calculated via a wind tunnel test although I would expect more that 2000N.
http://www.gimsonrobotics.co.uk/GLA-..._actuator.html
Here's the actuators been used, as said in the description they can move at up to 30mm/second. Although thats is far from quick the problem is overcome by having the link to the rod right next to the pivot point. So with a very short extension the wing can change angle quite severely.
One simple idea i had was to use two limit switches which would be activated by a pin mounted on the lower part of the connecting rod beneath the boot lid.
So when the button on the wheel is pushed the wing is activated to move in the positive direction as such and moves upwards until it reaches the upper limit switch at which point it stops.
Then when the brake pedal is pushed, maybe just through the brake lights a current could be taken to activate the actuators to move in the negative direction, once they reach the required air brake angle and trip the limit switch then the actuators stop again.
However this still leaves the problem of how to set a home position for when neither an input from the button or brake lights are received.
As mentioned above there's no real need for proportional control with this system as it basically can be said there is just positionA, B or C. Pick one! haha. Although there could be a system with proportional movement it would be far more complicated than what I'm at.
Only this morning I was questioning my choice to use two actuators, it is a problem. But the two are needed as the forces using the airbrake could be upwards of 2000N so there needs to be an element of factors of safety. Surely if there are limit switches though set in the same physical position then they would stay in check?
What do you mean by it would'nt fit the trunk?
To be honest the wing is very much over engineered for safety reasons so there will be little or no twist.
Once I am done this years college I'll be moving onto the rest of the aero bits on the car, it really is endless the amount you can do but its incredibly interesting. Bits will include a front splitter, new cooling system, flat floor and a diffuser. So plenty of work to be done, in the future
As said above they actuators used can move at 30mm/sec under load. To optimise the speed the connecting point on the wing will be located very close to the pivot point.
Although its not ideal it will do the job.
Severaly people have mentioned the gradual control before it raises some other issues as I like the idea of having an always home position as it acts as a safety as the wing always returns to the high downforce mode, giving optimum control unless another input is recieved form the push button or brake lights
As said above, hydraulics were ruled out as they raise a safety issue





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