Abstract
This paper provides a new method to nonlinear control theory, which is developed from the eigenvalue assignment method. The main purpose of this method is to locate the pointwise eigenvalues of the linear-like structure built by freezing the nonlinear systems at a given time instant in a desired disk region. Since the control requirements for the transient response characteristics are the major constraints on the selection of the disk centre and radius, two different update algorithms are also developed to reshape the disk region by changing the disk centre and radius at each time step. The effectiveness of the proposed methods is tested in both simulations and experiments. A validated three-DOF laboratory helicopter is used for experiments.
Original language | English |
---|---|
Article number | 893 |
Journal | Aerospace |
Volume | 10 |
Issue number | 10 |
DOIs | |
Publication status | Published - Oct 2023 |
Externally published | Yes |
Bibliographical note
Publisher Copyright:© 2023 by the authors.
Keywords
- 3-DOF helicopter
- nonlinear systems
- real-time control
- regional eigenvalue assignment
- robust control
- stability margin
- transient response