Abstract
This study addresses the adaptive and optimal control problem of a Quanser's 2-degree-of-freedom helicopter via output feedback. In order to satisfy the requirement of digital implementation of flight controller, this study distinguishes itself through proposing a novel sampled-data-based approximate/adaptive dynamic programming approach. A policy iteration algorithm is presented that yields to learn a near-optimal control gain iteratively by input/output data. The convergence of the proposed algorithm is theoretically ensured and the trade-off between the optimality and the sampling period is rigorously studied as well. Finally, the authors show the performance of the proposed algorithm under bounded model uncertainties.
Original language | English (US) |
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Pages (from-to) | 1440-1447 |
Number of pages | 8 |
Journal | IET Control Theory and Applications |
Volume | 10 |
Issue number | 12 |
DOIs | |
State | Published - Aug 8 2016 |
ASJC Scopus subject areas
- Control and Systems Engineering
- Human-Computer Interaction
- Computer Science Applications
- Control and Optimization
- Electrical and Electronic Engineering