Missile IGC Based on Improved Model Predictive Control and Sliding Mode Observer
Considering recurrent optimization process in model predictive control (MPC), the model uncertainties and disturbances terms in the missile’s guidance and control model can degrade recursive feasibility, and there are control mutation problems in common MPC algorithm. This paper presents a disturban...
Enregistré dans:
| Auteurs principaux: | Li Ma, Jiayuan Shan, Junhui Liu, Yan Ding |
|---|---|
| Format: | article |
| Langue: | EN |
| Publié: |
Hindawi Limited
2021
|
| Sujets: | |
| Accès en ligne: | https://doaj.org/article/68812ed41ccf43afb545e844271b0c71 |
| Tags: |
Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!
|
Documents similaires
-
Dual Quaternion Based Close Proximity Operation for In-Orbit Assembly via Model Predictive Control
par: Chuqi Sun, et autres
Publié: (2021) -
A Conflict Risk Analysis of MAV\UAV Flight in Shared Airspace
par: ChaoYu Xia, et autres
Publié: (2021) -
Research on the Fatigue of Small Impulse Turbine Blade Based on the Numerical Simulation and Experimental Tests
par: Shijie Liu, et autres
Publié: (2021) -
Interpolation-Based Modeling Methodology for Efficient Aeroelastic Control of a Folding Wing
par: Chengyu Yue, et autres
Publié: (2021) -
Numerical Study on Rod Thrust Vector Control for Physical Applications
par: Dong Li, et autres
Publié: (2021)