Hi Guys
Any one with any inputs on what contributes to good stable multirotor design?
I am looking for stability for AP work, not acrobatics.
Some questions I have in mind
1) All things equal, what is effect of increasing wheelbase / diameter? Perhaps there may be some optimum ratio / relationship
of wheelbase vs weight vs thrust per arm?
2) X and Y axis symmetry... Traditional MRs are symmetrical about XY axis, but what about those that are not,
like the 'dead cat' style quadcopter frame where its only symmetrical in one axis? I am guessing this just means that the Roll and Pitch gains
in FC will be different as opposed to exactly the same values for a symmetrical design?
3) I am building an octo coaxial X4. Now that its taking shape, I realise that since it has double motors on each arm (and I chose to have
the ESCs on the arms near the motors too)... now it seems to have more of its mass spread to the arms vs, mass being in centralised in the hub area.
Any pros and cons to this?
4) Choice of MASS of props? Non scientific one-off try...found that heavier wooden props led to more wobbly yaw movement on a hexa I had
vs lighter carbon props.
5) I was reading somewhere where some people say that a more stable config is to have centre of mass/weight above centre of pressure
(COP i am guessing refers to the centre of where the thrust originates?), ie, Z axis CG and its effects.
Any other thoughts?
Any one with any inputs on what contributes to good stable multirotor design?
I am looking for stability for AP work, not acrobatics.
Some questions I have in mind
1) All things equal, what is effect of increasing wheelbase / diameter? Perhaps there may be some optimum ratio / relationship
of wheelbase vs weight vs thrust per arm?
2) X and Y axis symmetry... Traditional MRs are symmetrical about XY axis, but what about those that are not,
like the 'dead cat' style quadcopter frame where its only symmetrical in one axis? I am guessing this just means that the Roll and Pitch gains
in FC will be different as opposed to exactly the same values for a symmetrical design?
3) I am building an octo coaxial X4. Now that its taking shape, I realise that since it has double motors on each arm (and I chose to have
the ESCs on the arms near the motors too)... now it seems to have more of its mass spread to the arms vs, mass being in centralised in the hub area.
Any pros and cons to this?
4) Choice of MASS of props? Non scientific one-off try...found that heavier wooden props led to more wobbly yaw movement on a hexa I had
vs lighter carbon props.
5) I was reading somewhere where some people say that a more stable config is to have centre of mass/weight above centre of pressure
(COP i am guessing refers to the centre of where the thrust originates?), ie, Z axis CG and its effects.
Any other thoughts?