我吃花盘旋
发表于 2025-3-28 14:35:04
Design of Deformable Flapping Structure of Bat-Like Flapping Air Vehicle folding and unfolding mechanism to achieve the goal of unfolding the wings to increase the lift during the downward and folding the wings to reduce the resistance during the upward. The motion function of 3D modeling flapping mechanism is verified by ADAMS. The results show that the structure meets
Oratory
发表于 2025-3-28 21:39:36
An Autonomous Flight Control Strategy Based on Human-Skill Imitation for Flapping-Wing Aerial VehiclV is hard to control precisely, because of its inherent vibration and complex dynamic analysis. Therefore, most FAV are controlled by human manipulators. In this paper, we mainly focus on studying the experience of human manipulators, using the experience to control our FAV, also known as HITHawk. W
animated
发表于 2025-3-28 23:36:36
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打折
发表于 2025-3-29 05:56:31
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痛苦一下
发表于 2025-3-29 09:00:01
Research on Technology of Pipeline Detection Robot Based on Spiral Propulsioncompact, functionally integrated micro pipeline inspection robot and the corresponding pipeline inspection and scanning strategy. First, the robot adopts the driving principle based on spiral propulsion, and uses only one power source to realize the robot‘s forward, backward, and stop motions in the
新娘
发表于 2025-3-29 15:27:33
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gain631
发表于 2025-3-29 15:50:16
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从容
发表于 2025-3-29 20:19:08
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Heterodoxy
发表于 2025-3-30 01:44:05
Hydrodynamic Coefficient Estimation of Small Autonomous Underwater Vehicle, the dynamic performance of the small AUVs is strongly affected by hydrodynamic effects. In this work, based on a novel designed small AUV, we conduct a hydrodynamic coefficients estimation work by adopting the computational fluid dynamics (CFD) method. Firstly, the resistance to AUV under differen
仔细阅读
发表于 2025-3-30 07:09:46
Stiffness Modeling of a Novel 2-DOF Solar Tracker with Consideration of Universal Joint Stiffnessl method to derive the stiffness matrix of universal joint in non-diagonal form is proposed. Considering the influence of universal joint stiffness on the deformation of solar tracker, the stiffness matrix of the solar tracker is derived with Matrix Structural Analysis method. The simulation on the