Lv1
30 积分 2025-07-09 加入
Analysis, optimization, and testing of a tilt-body aircraft
9个月前
已完结
Aerodynamic Performance of Propeller–Wing in Continuous Transition Mode Under Different Strategies
9个月前
已完结
Transition Performance Of Tilt Propeller Aircraft
9个月前
已关闭
Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion
1年前
已完结
Design and flight testing of flight control laws integrating incremental nonlinear dynamic inversion and servo current control
1年前
已完结
Transition Strategy Optimization of Tilt-Rotor VTOL UAV in Conversion Process
1年前
已完结
Agile and Precise Attitude Control of Tiltrotor Aircraft in Transition Flight
1年前
已完结
Angular acceleration estimation-based incremental nonlinear dynamic inversion for robust flight control
1年前
已关闭
Explicit Uncertainty Quantification for Probabilistic Assessment of Rotorcraft Handling Qualities
1年前
已关闭
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