Designing Backstepping Control System for Hypersonic Vehicle Based on Feedback Linearization
A hypersonic vehicle uses the airbreathing scramjet engine and the airframe and engine integrated design. Therefore, there is a strong cross-coupling effect among its aerodynamic force, thrust, structure, and control. The nonlinearity and uncertainty of the model cause difficulties in control system...
Saved in:
Main Authors: | Jianli Wei, Huan Chen |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2015-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2015/916328 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Backstepping Control Based on Constrained Command Filter for Hypersonic Flight Vehicles with AOA and Actuator Constraints
by: Junbao Wei, et al.
Published: (2021-01-01) -
Global Asymptotic Stability of Nonlinear Strict Feedback System via Backstepping Control Approach
by: Suka Garagara Kinwi, et al.
Published: (2023-01-01) -
Neural Network Backstepping Controller Design for Fractional-Order Nonlinear Systems
by: Youjun Chen, et al.
Published: (2021-01-01) -
Adaptive Neural Control of Hypersonic Vehicles with Actuator Constraints
by: Changxin Luo, et al.
Published: (2018-01-01) -
Disturbance Observer-Based Adaptive Control of Hypersonic Vehicles with Constrained Actuators
by: Guan Wang, et al.
Published: (2020-01-01)