Name
Title | ||
|---|---|---|
Fixed-Wing MAV Adaptive PD Control Based on a Modified MIT Rule with Sliding-Mode Control |
Abstract | ||
|---|---|---|
This paper presents an adaptive PD control law by using a modified MIT rule. The adaptation of the controller gains is based on the adjustment mechanism of the MIT rule by the gradient method with three types of sliding-mode control, i.e., first order sliding-mode control, second order sliding-mode (2SM), and high order sliding-mode control (HOSM). The proposed adjustment mechanism with the PD controller have been designed for the altitude movement, directional and lateral dynamics of a fixed-wing miniture aerial autonomous vehicle (MAV). Several simulations have been carried out in order to analyze the response of the modified MIT rule. |
Year | DOI | Venue |
|---|---|---|
2018 | https://doi.org/10.1007/s10846-018-0856-y | Journal of Intelligent and Robotic Systems |
Keywords | Field | DocType |
Adaptive control,Adjustment mechanism,Sliding mode control,PD controller | Wing,PID controller,Control theory,Control engineering,Adaptive control,Engineering,Sliding mode control,Aerodynamics | Journal |
Volume | Issue | ISSN |
91 | 1 | 0921-0296 |
ISBN | Citations | PageRank |
978-1-5090-4496-2 | 3 | 0.40 |
References | Authors | |
1 | 5 | |
Name | Order | Citations | PageRank |
|---|---|---|---|
| A. T. Espinoza-Fraire | 1 | 3 | 0.40 |
| Yangquan Chen | 2 | 2257 | 242.16 |
| A. Dzul | 3 | 237 | 32.31 |
| Rogelio Lozano | 4 | 914 | 166.62 |
| Juarez, R. | 5 | 4 | 1.47 |