@ Kelly
That should be calculated.
But take the IRIS-T missile as a reference.The picture has information that might interest you.
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@ Loathing
This static model is just this is a proof of concept.Therefore, some things are omitted because they are irrelevant in this type of test.
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@ Dan Griffing
I don't think it's possible to use the current principle of rolling stabilization for vertical stabilization and directional control.A completely different management system will be used for this vertical stabilization project that I am currently working on. This is a simple system to prevent the rocket from rolling, nothing more nothing less.
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@JimJarvis50
This is just a static test model, the canard deflection is large due to the low air velocity generated by the fan.The change in canard deflection must be linear with the acceleration of the rocket.
I will read all the pages you have published.
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@ jgavlik
I think the results would be better if there were no stupid legal restrictions on the use of some technologies.For example for vertical stabilization of rockets could be used laser beam riding.Aim the laser at the sky, and the rocket flies in a straight line.
One of the projects I'm working on outside of these shows is a laser point tracking system (Quadrant photodiode used).Which would be used in robotics or an automated guided vehicle.But it could be used to accurately return the rocket to the desired location if there were no legal limitations ...
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@ schworer
I think the RC heli gyro is not adequate for use in rocketry.
Since I'm not currently able to fire high power rockets,if you're interested, I could make (Lite version) rocket roll stabilization system at my own expense.
It's just up to you to put it in the rocket and fire it.