Physical properties of PlutoX

[NITIKA JAGGI]

Hello,
I am working on modelling PlutoX dynamics in MATLAB for which I need its physical properties. Kindly specify the total mass of assembled drone, dimensions, moment of inertia matrix, arm length from centre of mass for PlutoX.
Thank you,
Nitika.

[NITIKA JAGGI]

Kindly also provide details like aerodynamic coefficient & damping coefficient for the quad and damping coefficient & moment of inertia for the propellers.

Thank you,
Nitika.

[zn_pluto]

Hi,
The parameters of PlutoX are
Quadcopter mass- 56 g
Arm length- 65 mm
Moment of Inertia about x axis- 6.50E-05 Kgm2
Moment of Inertia about y axis- 6.21E-05 Kgm2
Moment of Inertia about z axis- 1.18E-04 Kgm2
Aerodynamic force coefficient- 2.83E-08 Ns2
Propeller inertia- 5.15E-07 Kgm2
The rest of the parameters will be updated later.

[NITIKA JAGGI]

Thank you for the prompt reply. Am eagerly waiting for the other parameters before I can proceed.

[zn_pluto]

The aerodynamic moment coefficient is 1.55E-10 Nms2(assumed)

• This reply was modified 3 years, 9 months ago by zn_pluto.

[NITIKA JAGGI]

Thanks a lot!

[NITIKA JAGGI]

Hello!
Kindly also provide the max rpm of the motors with the propellers attached.

Thank you,
Nitika.

[zn_pluto]

Hello,

The max rpm is 30000

[NITIKA JAGGI]

Thank you.

[Author]

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