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西北工业大学 国内
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The modeling and fine attitude control for aeroelastic hypersonic vehicle
Zhong Jie Meng
,
Jie Yan
航天学院
科研成果
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探究 'The modeling and fine attitude control for aeroelastic hypersonic vehicle' 的科研主题。它们共同构成独一无二的指纹。
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Engineering
Attitude Control
100%
Hypersonic Vehicle
100%
Angle-of-Attack
60%
Model Parameter
40%
Measurement Noise
20%
Control System
20%
Aerodynamics
20%
Simulation Result
20%
Control Strategy
20%
Actuator
20%
Active Control
20%
Flight Control
20%
Aerodynamic Model
20%
Rigid Structure
20%
Elastic Problem
20%
Physics
Attitude Control
100%
Hypersonic Vehicle
100%
Angle of Attack
60%
Noise Measurement
20%
Actuator
20%
Active Control
20%
Flight Control
20%
Aerodynamics
20%
Rigid Structure
20%
Supersonic Combustion Ramjet Engine
20%
Aerodynamic Heating
20%
Linear Quadratic Regulator
20%