Guidance law and neural control for hypersonic missile to track targets
From MaRDI portal
Publication:1723704
DOI10.1155/2016/6219609zbMath1417.93201OpenAlexW2327159227WikidataQ59123597 ScholiaQ59123597MaRDI QIDQ1723704
Jie Yan, Binbin Yan, Xiaofei Chang, Wenxing Fu
Publication date: 19 February 2019
Published in: Discrete Dynamics in Nature and Society (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1155/2016/6219609
Cites Work
- Unnamed Item
- Composite fuzzy control of a class of uncertain nonlinear systems with disturbance observer
- Sliding modes in control and optimization. Transl. from the Russian
- Controlling nonlinear time-varying systems via Euler approximations
- Smooth second-order sliding modes: missile guidance application
- Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity
- Adaptive discrete-time controller design with neural network for hypersonic flight vehicle via back-stepping
- Design of Robust Control Systems for a Hypersonic Aircraft
- Multirate Output Feedback Based Robust Quasi-Sliding Mode Control of Discrete-Time Systems
- Application of discrete time sliding mode control to a spacecraft in 6DoF with parameter identification
- Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation
- Nonlinear adaptive control using neural networks and multiple models
This page was built for publication: Guidance law and neural control for hypersonic missile to track targets