標(biāo)題: Titlebook: Proceedings of the 19th International Conference on Intelligent Unmanned Systems; ICIUS 2023, 5–7 July Rini Akmeliawati,David Harvey,Hoon C [打印本頁(yè)] 作者: 日月等 時(shí)間: 2025-3-21 18:18
書目名稱Proceedings of the 19th International Conference on Intelligent Unmanned Systems影響因子(影響力)
書目名稱Proceedings of the 19th International Conference on Intelligent Unmanned Systems影響因子(影響力)學(xué)科排名
書目名稱Proceedings of the 19th International Conference on Intelligent Unmanned Systems網(wǎng)絡(luò)公開度
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書目名稱Proceedings of the 19th International Conference on Intelligent Unmanned Systems讀者反饋
書目名稱Proceedings of the 19th International Conference on Intelligent Unmanned Systems讀者反饋學(xué)科排名
作者: 護(hù)航艦 時(shí)間: 2025-3-21 21:43
Conference proceedings 2024manned Systems (ICIUS 2023), which was held in Adelaide, Australia, on 5–7 July 2023. The book is composed of articles that cover the advanced progress in unmanned systems, such as bio-inspired, underwater, aerial, and off-earth systems, as well as their subsystems, including control and navigation,作者: GORGE 時(shí)間: 2025-3-22 01:02 作者: 反話 時(shí)間: 2025-3-22 04:33
Leading-Edge Twisting Mechanisms for Flapping Wingsere fabricated using the fused deposition modeling (FDM) 3D printing. They are type-A1 (normal servo) mechanism for simple flapping motion, type-B (servo-bevel gear) mechanism for flapping with continuous leading-edge twisting, and type-B1 (servo-bevel gear with adjustable mechanical stopper) mechan作者: NOVA 時(shí)間: 2025-3-22 10:18
Aerodynamics and Control of an Ornithopter with a Bird-Like Tail achieve stability and control during flight. Birds, in contrast, are very proficient in directional control by using their tail in which there is no vertical tail or neither a ‘V’ tail. The absence of a vertical tail in a conventional aircraft would cause severe control and stability problems. Diff作者: addict 時(shí)間: 2025-3-22 15:08 作者: Forage飼料 時(shí)間: 2025-3-22 18:51
Autonomous Control Design for a Two-Wing Tailless Flapping-Wing Micro Air Vehicle Systemsumption and long flight times due to the flapping wing design. However, these designs have inherent instability, due to having only two control surfaces, which are also responsible for providing lift. This work attempts to implement a flight control system (FCS) for a two-wing tailless FW-MAV using作者: 控訴 時(shí)間: 2025-3-23 00:05
Control Board Design for a Directly Motor-Driven Flapping MAVosed FWMAV are driven directly by two DC motors and extension springs are used to store and release inertial energy at each flapping direction inverting. To get better energy efficiency, the natural frequency of flapping wings can be adjusted by tuning spring constant and transmission gear ratio. Co作者: 離開就切除 時(shí)間: 2025-3-23 02:19
CaveX: A Low-Impact Robust Cave Mapping Hexapod Robotd scientific research, with continuing project development toward full autonomy. . The CaveX robot is a biologically-inspired hexapod which uses LiDAR (Light Detection And Ranging) sensing to explore and map cave systems while minimising its environmental footprint. It comprises five subsystems—sens作者: 懦夫 時(shí)間: 2025-3-23 07:19
Bio-inspired Legged Robot for Space Exploration effectively traversed through the application of unique movement patterns used by animals. This paper presents a hopping robot that imitates the bipedal hopping and pentapedal bounding gaits of a kangaroo for the purpose of interplanetary exploration. The gravitational accelerations of other planet作者: dura-mater 時(shí)間: 2025-3-23 12:51
Development of Unmanned Surface Vehicle for In-Situ Water Quality Measurement Using IoTams and rivers is necessary to examine the water contaminants. The present work focused on developing an Unmanned Surface Vehicle (USV) to collect water samples in remote water body locations. . A solenoid-actuated water sampling system with an automatic cutoff of storage was devised. In addition, a作者: RECUR 時(shí)間: 2025-3-23 14:11
Simulation and Controller Design of an Underwater Vehicleents, including scientific research, ocean mapping, environmental monitoring, and military applications. Their main purpose is to operate the underwater vehicle autonomously without requiring a human pilot, which allows them to collect data in dangerous or difficult-to-reach areas, operate for exten作者: Alcove 時(shí)間: 2025-3-23 20:48
Neuroevolutionary Reinforcement Learning of an Autonomous Underwater Vehicle in Confined Spaceo test the intelligent system under various situations or edge cases. While the application of artificial intelligence in the design of road-based vehicles has advanced to the level of self-driving vehicles, there is still a substantial research gap on AUVs that operate in constrained areas, such as作者: BATE 時(shí)間: 2025-3-24 01:47 作者: Indelible 時(shí)間: 2025-3-24 04:02 作者: 使成波狀 時(shí)間: 2025-3-24 06:32 作者: acrimony 時(shí)間: 2025-3-24 12:10
A Hybrid-Type Power Transmission Line Inspection Drone and an Anomaly Detection Method Using a Deep Neural Networkpower transmission lines are one of the crucial infrastructures for our society, their regular maintenance and damage assessment are required. Manual inspections are currently performed by human workers who climb up transmission towers and navigate through the lines, which is time-consuming and pose作者: 對(duì)待 時(shí)間: 2025-3-24 15:37
Designing Mining Robot for Swarm Rover Fleet Carrying Out Water Extraction on the Moononcept has been proposed which implies extracting and using resources from asteroids, the Moon and other planets. Water is an important resource for sustaining long-term manned missions and mining activities on the Moon. The unpredictability of space mining requires careful development of mining met作者: PLIC 時(shí)間: 2025-3-24 20:26
Investigating the?Use of?Electrodynamic Dust Shielding to?Improve the?Robustness of?a?Lunar Rover Drivetrain to?Regolith (EDS), as it is not possible to manually clean such systems. The EDS may be used to reduce the volume of regolith incident on passive dust mitigation and dust tolerant designs for lunar rover drive systems, increasing rovers’ effectiveness and longevity that would otherwise be decreased by dust sca作者: 白楊 時(shí)間: 2025-3-24 23:58 作者: irradicable 時(shí)間: 2025-3-25 05:21
1876-1100 ogress in unmanned systems, such as bio-inspired, underwater.This book contains selected high-quality reviewed papers that have been accepted and presented at the 19th International Conference of Intelligent Unmanned Systems (ICIUS 2023), which was held in Adelaide, Australia, on 5–7 July 2023. The 作者: 一條卷發(fā) 時(shí)間: 2025-3-25 10:41 作者: 假 時(shí)間: 2025-3-25 15:04
Mochammad Agoes Moelyadi,Syahrahman A. Ginting,Oktavianus Demas Priambudi,Dzikrian Diqnada,Prayoga,Asiah Annur Sarhani作者: Bouquet 時(shí)間: 2025-3-25 17:35 作者: 是貪求 時(shí)間: 2025-3-25 23:35 作者: OTHER 時(shí)間: 2025-3-26 01:12 作者: Landlocked 時(shí)間: 2025-3-26 05:26
Development of Bio-inspired Perforated Flapping Wings the proposed wing design, demonstrating its potential for the development of more efficient and effective ornithopters. This approach provides a new direction for ornithopter wing design and offers potential for applications in various fields.作者: Virtues 時(shí)間: 2025-3-26 08:29 作者: Ruptured-Disk 時(shí)間: 2025-3-26 14:28
Development of Unmanned Surface Vehicle for In-Situ Water Quality Measurement Using IoTenabled USV is an efficient choice for online monitoring of water quality parameters. The USV was also tested for its stability on the water surface under various wind loads, and it was able to withstand the wind conditions for effective water sampling and in-situ water quality measurements.作者: Blasphemy 時(shí)間: 2025-3-26 17:11
Simulation and Controller Design of an Underwater Vehiclezed. It is found that both controllers have big gain margins and 45-degree phase margins. The bandwidth of the pitch control loop and yaw control loops are 4?rad/s and 0.3?rad/s, respectively. Both step responses show that the steady-state errors and maximum overshoot are very small.作者: GLARE 時(shí)間: 2025-3-27 00:33 作者: Inscrutable 時(shí)間: 2025-3-27 04:47 作者: urethritis 時(shí)間: 2025-3-27 06:54 作者: sterilization 時(shí)間: 2025-3-27 09:56
Leading-Edge Twisting Mechanisms for Flapping Wings understanding the corresponding lift force value. Furthermore, a theoretical rigid body dynamics was applied to create the 2D profile and verify the 2D cut sections from MATLAB. The comprehensive study and evaluation of lift and net thrust forces due to leading-edge twisting were conducted for all three flapping mechanisms in this study.作者: 纖細(xì) 時(shí)間: 2025-3-27 16:12
Modelling and Simulation of Fluid–Structure Interaction for Piezoelectric Energy Harvesting in Simplified HALE UAV Wingsmic structure and fluid flow behavior. The result of this analysis illustrates that energy harvesting from transient vibration may provide adequate energy to support onboard sensor and electrical system during UAV operation.作者: addict 時(shí)間: 2025-3-27 20:15
