Abstract
This paper deals with canonical normal form approach for trajectory tracking control of a two degree-of-freedom helicopter system. The main objective is to stabilize beam of the helicopter with respect to pitch and yaw angles. Sufficient geometrical conditions are given for a class of nonlinear dynamical systems to transform the studied nonlinear systems into a triangular normal form and determine the flat outputs. Using this form two controllers are designed to control the position of the yaw and the pitch angles of the Helicopter. Simulation results are given to illustrate the effectiveness of the proposed control scheme.
| Original language | English |
|---|---|
| Title of host publication | 18th IEEE International Multi-Conference on Systems, Signals and Devices, SSD 2021 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 765-770 |
| Number of pages | 6 |
| ISBN (Electronic) | 9781665414937 |
| DOIs | |
| State | Published - 22 Mar 2021 |
| Externally published | Yes |
Publication series
| Name | 18th IEEE International Multi-Conference on Systems, Signals and Devices, SSD 2021 |
|---|
Bibliographical note
Publisher Copyright:© 2021 IEEE.
Keywords
- 2DOF
- Flatness
- Nonlinear systems
- Normal Form
ASJC Scopus subject areas
- Artificial Intelligence
- Computer Networks and Communications
- Computer Science Applications
- Signal Processing
- Electrical and Electronic Engineering