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西北工业大学 国内
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Dynamic-Command-Limiting-Based AOA Constraint Control of Hypersonic Flight Vehicle
Shuai Liang,
Bin Xu
, Shaoshan Sun, Chenggang Tao
自动化学院
Xi'an University of Technology
Northwestern Polytechnical University Xian
China Aviation Industry Corporation
科研成果
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2
引用 (Scopus)
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探究 'Dynamic-Command-Limiting-Based AOA Constraint Control of Hypersonic Flight Vehicle' 的科研主题。它们共同构成独一无二的指纹。
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Engineering
Angle-of-Attack
100%
Hypersonic Flight Vehicle
100%
Control Constraint
100%
Control System
28%
System Protection
28%
Simulation Result
14%
Closed Loop
14%
Limitations
14%
Maneuverability
14%
Constant Value
14%
Control Scheme
14%
Initial State
14%
Loop Dynamic
14%
Physics
Angle of Attack
100%
Hypersonic Flight
100%
Protection System
28%
Maneuverability
14%
Feedback
14%
Computer Science
Remaining Angle
50%
Constant Value
50%