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西北工业大学 国内
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Novel Adaptive Saturated Attitude Tracking Control of Rigid Spacecraft with Guaranteed Transient and Steady-State Performance
Zeyang Yin,
Jianjun Luo
, Caisheng Wei
航天学院
Northwestern Polytechnical University Xian
科研成果
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引用 (Scopus)
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探究 'Novel Adaptive Saturated Attitude Tracking Control of Rigid Spacecraft with Guaranteed Transient and Steady-State Performance' 的科研主题。它们共同构成独一无二的指纹。
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Engineering
Transients
100%
Prescribed Performance
100%
Control Scheme
75%
Attitude Control
50%
Illustrates
25%
Convergence Rate
25%
External Disturbance
25%
Dynamic Programming
25%
Boundedness
25%
Inertia Matrix
25%
Saturation Nonlinearity
25%