scholarly journals Design and control of a two-degree-of-freedom lightweight flexible arm

Author(s):  
V. Feliu ◽  
K.S. Rattan ◽  
H.B. Brown
1989 ◽  
Author(s):  
Vincente Feliu ◽  
H. B. Brown ◽  
Rattan Jr. ◽  
Kuldip S.

1998 ◽  
Vol 64 (620) ◽  
pp. 1382-1389 ◽  
Author(s):  
Kouji OKUDA ◽  
Kazuyuki KUHARA ◽  
Minoru SASAKI ◽  
Fumio FUJISAWA

2011 ◽  
Vol 403-408 ◽  
pp. 4649-4658 ◽  
Author(s):  
Pouya Ghalei ◽  
Alireza Fatehi ◽  
Mohamadreza Arvan

Input-Output data modeling using multi layer perceptron networks (MLP) for a laboratory helicopter is presented in this paper. The behavior of the two degree-of-freedom platform exemplifies a high order unstable, nonlinear system with significant cross-coupling between pitch and yaw directional motions. This paper develops a practical algorithm for identifying nonlinear autoregressive model with exogenous inputs (NARX) and nonlinear output error model (NOE) through closed loop identification. In order to collect input-output identifier pairs, a cascade state feedback (CSF) controller is introduced to stabilize the helicopter and after that the procedure of system identification is proposed. The estimated models can be utilized for nonlinear flight simulation and control and fault detection studies.


2007 ◽  
Vol 40 (14) ◽  
pp. 109-114
Author(s):  
Nikolai N. Bolotnik ◽  
Mikhail Pivovarov ◽  
Igor Zeidis ◽  
Klaus Zimmermann

Author(s):  
T-J Yeh ◽  
C-Y Su ◽  
W-J Wang

This paper investigates modelling and control issues associated with a two-degree-of-freedom inertial platform for naval applications. In the modelling part, the dynamics of the system are physically characterized and then experimentally identified. It is found that due to the inverted-pendulum structure and the use of hydraulic actuators, the system is open-loop unstable and exhibits different frequency responses when the amplitude of the input signal changes. Moreover, the identification experiment reveals that the inclinometer used has a major resonant peak that will limit the control system performance. Therefore, a complimentary filter scheme is proposed to condition the sensor signals so as to produce a more acceptable absolute-angle measurement. In the control part, two proportional-integral-derivative (PID) controllers, whose control parameters are computed using a non-linear optimization scheme to achieve optimal disturbance rejection with reasonable robustness and noise sensitivity properties, are respectively designed for the pitch and the roll subsystems. Experimental results indicate that when the platform's base frame encounters a biaxial sea-wave motion, the resulted control system can attenuate the vibration to within 10 per cent.


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