Title :
Dynamic modelling and control of a 2-DOF twin rotor multi-input multi-output system
Author :
Ahmad, S.M. ; Chipperfield, A.J. ; Tokhi, M.O.
Author_Institution :
Dept. of Autom. Control & Syst. Eng., Univ. of Sheffield, UK
Abstract :
A dynamic model for the characterisation of a two-degree-of-freedom (DOF) twin rotor MIMO system (TRMS) in hover is extracted using a black-box system identification technique. Its behaviour in certain aspects resembles that of a helicopter, with a significant cross-coupling between longitudinal and lateral directional motions. The extracted model is employed for designing and implementing a feedforward/open-loop control. Open-loop control is often the preliminary step for development of more complex feedback control laws. Hence, this paper also investigates open-loop control strategies using shaped command inputs for resonance suppression in the TRMS. Digital low-pass and band-stop shaped inputs are used on the TRMS testbed, based on the identified vibrational modes. A comparative performance study is carried out and the results presented. The low-pass filter is shown to exhibit better vibration reduction. When modal coupling exists, decoupled feedback controllers are incapable of eliminating vibration. in such cases, generating motion by shaped reference inputs is clearly advantageous
Keywords :
MIMO systems; discrete time systems; dynamics; feedforward; flexible structures; helicopters; identification; vibration control; discrete-time system; dynamics; feedforward; flexible structures; helicopter; identification; linear identification; low-pass filter; open-loop control; transfer function; twin rotor MIMO system; vibration control; Feedback control; Helicopters; Low pass filters; MIMO; Open loop systems; Resonance; Shape control; System identification; Testing; Transmission line measurements;
Conference_Titel :
Industrial Electronics Society, 2000. IECON 2000. 26th Annual Confjerence of the IEEE
Conference_Location :
Nagoya
Print_ISBN :
0-7803-6456-2
DOI :
10.1109/IECON.2000.972335