Dossier Histórico Modelístico, Primera Versión, TWIN OTTER Grupo N° 6 de la Fuerza Aérea chilena
MIMO
MIMO
manual mimoFull description
Descripción completa
Experiment: - Twin Rotor MIMO System.
Objective Observation:-
Procedure:$. Firstly, system simulation run and a nd observed the system behavior. The inputs were a pplied to pitch and yaw in non linearity with sin wave input and a nd step input. The non linearity sin and an d step input as follows. Pitch
yaw
Sin
Sin
Sin
Step
Step
Sin
Step
Step
And then separately to Sin and a nd step input only to Pitch and a nd Yaw.
Observations:-
The Model system
For the Sin to Pitch and Yaw I)
Pitch elevation
II)
Yaw azimuth
For the Step to Pitch and Sine toYaw
Pitch elevation
Yaw azimuth
For Sine to Pitch & Step to Yaw
Appling step only to Pitch.
Appling Sine only to Pitch
Appling Sine only to Yaw
Used
2DOF model
Model
Step Step input both Pith & Yaw
Pitch
to Step & Yow to Sine
Pitch
to Sine & Yow to Step
Pitch
to Sine & Step to Yow
Appling PID values to control model. (Pitch)
PID values.
Step input with PID values (3,8,10) respect to PID