Flight-Propulsion Integration Dynamic Analysis and Adaptive Control of the Hypersonic Vehicle at Wide-Range Mach Numbers.
Jiaxin LiDanwei LiGuoqiang WuKai LiuPublished in: IEEE Access (2022)
Keyphrases
- wind tunnel
- nasa langley research center
- adaptive control
- dynamic analysis
- wide range
- static analysis
- reverse engineering
- nonlinear systems
- feedback control
- control method
- flight test
- dynamic environments
- technology transfer
- flight control
- control law
- reinforcement learning
- adaptive controller
- variable structure
- data integration
- control system
- autonomous control
- model checking
- source code
- least squares
- database systems
- real time
- closed loop
- machine learning