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2024-10-10 加入
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Attitude Control of Flapping-Wing Micro Air Vehicles Based on Hyperbolic Tangent Function Sliding Mode Control
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Combination of terminal sliding mode and finite-time state-dependent Riccati equation: Flapping-wing flying robot control
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Design and comparison of tails for bird-scale flapping-wing robots
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An All Servo-Driven Bird-Like Flapping-Wing Aerial Robot Capable of Autonomous Flight
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Modeling the Bio-Inspired Wing-Tail Interaction Mechanism and Applying It in Flapping Wing Aircraft Pitch Control
1个月前
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