Reentry Attitude Control for RLV Based on Adaptive Event-Triggered Sliding Mode
An adaptive event-triggered sliding mode control (AETSMC) algorithm is designed for the attitude control of the Reusable Launch Vehicle (RLV) subject to unknown external disturbances. First, an AETSMC strategy for a multi-variable second-order nonlinear system is proposed. Then, the stability of the...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
IEEE
2019-01-01
|
| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/8718674/ |