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Distributed event-triggered collision avoidance coordinated control for QUAVs based on flexible virtual tubes
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作者 Hongzhen GUO Mou CHEN +1 位作者 Mihai LUNGU Baomin LI 《Chinese Journal of Aeronautics》 2025年第2期339-352,共14页
In this paper,a distributed Event-Triggered(ET)collision avoidance coordinated control for Quadrotor Unmanned Aerial Vehicles(QUAVs)is proposed based on Virtual Tubes(VTs)with flexible boundaries in the presence of un... In this paper,a distributed Event-Triggered(ET)collision avoidance coordinated control for Quadrotor Unmanned Aerial Vehicles(QUAVs)is proposed based on Virtual Tubes(VTs)with flexible boundaries in the presence of unknown external disturbances.Firstly,VTs are constructed for each QUAV,and the QUAV is restricted into the corresponding VT by the artificial potential field,which is distributed around the boundary of the VT.Thus,the collisions between QUAVs are avoided.Besides,the boundaries of the VTs are flexible by the modification signals,which are generated by the self-regulating auxiliary systems,to make the repulsive force smaller and give more buffer space for QUAVs without collision.Then,a novel ET mechanism is designed by introducing the concept of prediction to the traditional fixed threshold ET mechanism.Furthermore,a disturbance observer is proposed to deal with the adverse effects of the unknown external disturbance.On this basis,a distributed ET collision avoidance coordinated controller is proposed.Then,the proposed controller is quantized by the hysteresis uniform quantizer and then sent to the actuator only at the ET instants.The boundedness of the closed-loop signals is verified by the Lyapunov method.Finally,simulation and experimental results are performed to demonstrate the superiority of the proposed control method. 展开更多
关键词 Quadrotor unmanned aerial vehicles Collision avoidance Virtual tubes with flexible boundaries Event-triggered mechanism Hysteresis uniform quantizer Distributed coordinated control
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Safe flight corridor constrained sequential convex programming for efficient trajectory generation of fixed-wing UAVs 被引量:2
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作者 Jing SUN Guangtong XU +2 位作者 Zhu WANG Teng LONG Jingliang SUN 《Chinese Journal of Aeronautics》 2025年第1期537-550,共14页
Generating dynamically feasible trajectory for fixed-wing Unmanned Aerial Vehicles(UAVs)in dense obstacle environments remains computationally intractable.This paper proposes a Safe Flight Corridor constrained Sequent... Generating dynamically feasible trajectory for fixed-wing Unmanned Aerial Vehicles(UAVs)in dense obstacle environments remains computationally intractable.This paper proposes a Safe Flight Corridor constrained Sequential Convex Programming(SFC-SCP)to improve the computation efficiency and reliability of trajectory generation.SFC-SCP combines the front-end convex polyhedron SFC construction and back-end SCP-based trajectory optimization.A Sparse A^(*)Search(SAS)driven SFC construction method is designed to efficiently generate polyhedron SFC according to the geometric relation among obstacles and collision-free waypoints.Via transforming the nonconvex obstacle-avoidance constraints to linear inequality constraints,SFC can mitigate infeasibility of trajectory planning and reduce computation complexity.Then,SCP casts the nonlinear trajectory optimization subject to SFC into convex programming subproblems to decrease the problem complexity.In addition,a convex optimizer based on interior point method is customized,where the search direction is calculated via successive elimination to further improve efficiency.Simulation experiments on dense obstacle scenarios show that SFC-SCP can generate dynamically feasible safe trajectory rapidly.Comparative studies with state-of-the-art SCP-based methods demonstrate the efficiency and reliability merits of SFC-SCP.Besides,the customized convex optimizer outperforms off-the-shelf optimizers in terms of computation time. 展开更多
关键词 Fixed-wing unmanned aerial vehicle Efficient trajectory planning Safe flight corridor Sequential convex programming Customized convex optimizer
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Multiple fixed-wing UAVs collaborative coverage 3D path planning method for complex areas
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作者 Mengyang Wang Dong Zhang +1 位作者 Chaoyue Li Zhaohua Zhang 《Defence Technology(防务技术)》 2025年第5期197-215,共19页
Complex multi-area collaborative coverage path planning in dynamic environments poses a significant challenge for multi-fixed-wing UAVs(multi-UAV).This study establishes a comprehensive framework that incorporates UAV... Complex multi-area collaborative coverage path planning in dynamic environments poses a significant challenge for multi-fixed-wing UAVs(multi-UAV).This study establishes a comprehensive framework that incorporates UAV capabilities,terrain,complex areas,and mission dynamics.A novel dynamic collaborative path planning algorithm is introduced,designed to ensure complete coverage of designated areas.This algorithm meticulously optimizes the operation,entry,and transition paths for each UAV,while also establishing evaluation metrics to refine coverage sequences for each area.Additionally,a three-dimensional path is computed utilizing an altitude descent method,effectively integrating twodimensional coverage paths with altitude constraints.The efficacy of the proposed approach is validated through digital simulations and mixed-reality semi-physical experiments across a variety of dynamic scenarios,including both single-area and multi-area coverage by multi-UAV.Results show that the coverage paths generated by this method significantly reduce both computation time and path length,providing a reliable solution for dynamic multi-UAV mission planning in semi-physical environments. 展开更多
关键词 Multi-fixed-wing UAVs(multi-UAV) Minimum time cooperative coverage Dynamic complete coverage path planning(DCCPP) Dubins curves Improved dynamic programming algorithm(IDP)
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Low-profile,low sidelobe array antenna with ultrawide beam coverage for UAV communication 被引量:1
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作者 Mei LI Zhiliang SHANG +2 位作者 Lin PU Ming-Chun TANG Lei ZHU 《Chinese Journal of Aeronautics》 2025年第1期444-454,共11页
This paper presents a design method to implement an antenna array characterized by ultra-wide beam coverage,low profile,and low Sidelobe Level(SLL)for the application of Unmanned Aerial Vehicle(UAV)air-to-ground commu... This paper presents a design method to implement an antenna array characterized by ultra-wide beam coverage,low profile,and low Sidelobe Level(SLL)for the application of Unmanned Aerial Vehicle(UAV)air-to-ground communication.The array consists of ten broadside-radiating,ultrawide-beamwidth elements that are cascaded by a central-symmetry series-fed network with tapered currents following Dolph-Chebyshev distribution to provide low SLL.First,an innovative design of end-fire Huygens source antenna that is compatible with metal ground is presented.A low-profile,half-mode Microstrip Patch Antenna(MPA)is utilized to serve as the magnetic dipole and a monopole is utilized to serves as the electric dipole,constructing the compact,end-fire,grounded Huygens source antenna.Then,two opposite-oriented end-fire Huygens source antennas are seamlessly integrated into a single antenna element in the form of monopole-loaded MPA to accomplish the ultrawide,broadside-radiating beam.Particular consideration has been applied into the design of series-fed network as well as antenna element to compensate the adverse coupling effects between elements on the radiation performance.Experiment indicates an ultrawide Half-Power Beamwidth(HPBW)of 161°and a low SLL of-25 dB with a high gain of 12 d Bi under a single-layer configuration.The concurrent ultrawide beamwidth and low SLL make it particularly attractive for applications of UAV air-to-ground communication. 展开更多
关键词 Array antenna Broad beam Fan beam Low sidelobe level Chebyshev synthesis UAV communication
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基于Event模型的城市物流无人机同高度交叉运行间隔研究
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作者 张健 赵嶷飞 +2 位作者 卢飞 黎宗孝 罗鑫悦 《中国安全科学学报》 北大核心 2025年第5期99-105,共7页
为解决城市物流无人机飞行流量加大、隔离航线模式空域利用率低的矛盾,需要实施安全有效的交叉运行。通过研究交叉运行碰撞风险,确定侧向误差、垂直误差、纵向临近率等核心参数,构建同高度交叉运行间隔模型。在此基础上,进一步考虑机载... 为解决城市物流无人机飞行流量加大、隔离航线模式空域利用率低的矛盾,需要实施安全有效的交叉运行。通过研究交叉运行碰撞风险,确定侧向误差、垂直误差、纵向临近率等核心参数,构建同高度交叉运行间隔模型。在此基础上,进一步考虑机载冲突探测与解脱(CDR)系统失效问题,并运用事件树分析方法,提出并构建城市物流无人机交叉间隔综合模型。结果表明:在航线夹角为60°情况下,对标安全目标水平1.5×10^(-8),所需交叉间隔为158 m;对标安全目标水平1×10^(-6),所需交叉间隔155 m。随着交叉角度增大,运行间隔总体呈现上升趋势,当接近180°时,即对头运行时,所需间隔急剧上升,与实际认知一致。 展开更多
关键词 Event模型 城市物流无人机(UAV) 同高度 交叉运行 交叉间隔 冲突探测与解脱(CDR)
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Fault-observer-based iterative learning model predictive controller for trajectory tracking of hypersonic vehicles 被引量:1
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作者 CUI Peng GAO Changsheng AN Ruoming 《Journal of Systems Engineering and Electronics》 2025年第3期803-813,共11页
This work proposes the application of an iterative learning model predictive control(ILMPC)approach based on an adaptive fault observer(FOBILMPC)for fault-tolerant control and trajectory tracking in air-breathing hype... This work proposes the application of an iterative learning model predictive control(ILMPC)approach based on an adaptive fault observer(FOBILMPC)for fault-tolerant control and trajectory tracking in air-breathing hypersonic vehicles.In order to increase the control amount,this online control legislation makes use of model predictive control(MPC)that is based on the concept of iterative learning control(ILC).By using offline data to decrease the linearized model’s faults,the strategy may effectively increase the robustness of the control system and guarantee that disturbances can be suppressed.An adaptive fault observer is created based on the suggested ILMPC approach in order to enhance overall fault tolerance by estimating and compensating for actuator disturbance and fault degree.During the derivation process,a linearized model of longitudinal dynamics is established.The suggested ILMPC approach is likely to be used in the design of hypersonic vehicle control systems since numerical simulations have demonstrated that it can decrease tracking error and speed up convergence when compared to the offline controller. 展开更多
关键词 hypersonic vehicle actuator fault tracking control iterative learning control(ILC) model predictive control(MPC) fault observer
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Collision-inducing method for UAV evasive maneuvers based on receding horizon optimization
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作者 Haonan Tang Zhigong Tang +1 位作者 Gong Chen Jifeng Guo 《Defence Technology(防务技术)》 2025年第8期141-154,共14页
Aiming at the missile avoidance problem of the unmanned aerial vehicle(UAV)in complex obstacle environments,this work proposes a collision-avoidance method based on receding horizon optimization.The proposed method ge... Aiming at the missile avoidance problem of the unmanned aerial vehicle(UAV)in complex obstacle environments,this work proposes a collision-avoidance method based on receding horizon optimization.The proposed method generated a specific trajectory for the UAV to effectively induce the proportional navigation missile to successfully intercept the obstacle,thereby accomplishing the evasive maneuver.The evasive maneuver was divided into two distinct stages,namely the collision-inducing phase and the fast departure phase.The obstacle potential field-based target selection algorithm was employed to identify the most appropriate target obstacle,while the induced trajectory was determined through a combination of receding horizon optimization and the hp-adaptive pseudo-spectral method.Simulation experiments were carried out under three different types of obstacle environments and one multiobstacle environment,and the simulation results show that the method proposed in this paper greatly improves the success rate of UAV evasive maneuvers,proving the effectiveness of this method. 展开更多
关键词 UAV MISSILE Proportional navigation Evasive maneuver Receding horizon optimization Hp-adaptive pseudo-spectral method
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Regular virtual tube for cooperative transportation of a payload by multiple quadrotors
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作者 TANG Jiacheng YANG Zixiao +2 位作者 ZHANG Lei HU Tianjiang ZHU Bo 《Journal of Systems Engineering and Electronics》 2025年第4期1068-1076,共9页
How multi-unmanned aerial vehicles(UAVs)carrying a payload pass an obstacle-dense environment is practically important.Up to now,there have been few results on safe motion planning for the multi-UAVs cooperative trans... How multi-unmanned aerial vehicles(UAVs)carrying a payload pass an obstacle-dense environment is practically important.Up to now,there have been few results on safe motion planning for the multi-UAVs cooperative transportation system(CTS)to pass through such an environment.The prob-lem is challenging because it is difficult to analyze and explicitly take into account the swing motion of the payload in planning.In this paper,a modeling method of virtual tube is proposed by fus-ing the advantages of the existing modeling algorithm for regu-lar virtual tube and the expansion environment method.The pro-posed method can not only generate a safe and smooth tube for UAVs,but also ensure the payload stays away from the dense obstacles.Simulation results show the effectiveness of the method and the safety of the planned tube. 展开更多
关键词 virtual tube multi-unmanned aerial vehicles(UAVs) motion planning cooperative transportation system expansion environment anti swing.
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A multi-parametric path planning framework utilizing airspace visibility graphs for urban battlefield environments
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作者 Sidao Chen Xuejun Zhang +1 位作者 Zuyao Zhang Jianxiang Ma 《Defence Technology(防务技术)》 2025年第9期112-126,共15页
Urban combat environments pose complex and variable challenges for UAV path planning due to multidimensional factors,such as static and dynamic obstructions as well as risks of exposure to enemy detection,which threat... Urban combat environments pose complex and variable challenges for UAV path planning due to multidimensional factors,such as static and dynamic obstructions as well as risks of exposure to enemy detection,which threaten flight safety and mission success.Traditional path planning methods typically depend solely on the distribution of static obstacles to generate collision-free paths,without accounting for constraints imposed by enemy detection and strike capabilities.Such a simplified approach can yield safety-compromising routes in highly complex urban airspace.To address these limitations,this study proposes a multi-parameter path planning method based on reachable airspace visibility graphs,which integrates UAV performance constraints,environmental limitations,and exposure risks.An innovative heuristic algorithm is developed to balance operational safety and efficiency by both exposure risks and path length.In the case study set in a typical mixed-use urban area,analysis of airspace visibility graphs reveals significant variations in exposure risk at different regions and altitudes due to building encroachments.Path optimization results indicate that the method can effectively generate covert and efficient flight paths by dynamically adjusting the exposure index,which represents the likelihood of enemy detection,and the path length,which corresponds to mission execution time. 展开更多
关键词 UAV Path planning Urban battlefield environment Airspace visibility graph ISOVIST
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Outdoor navigation of millimeter-wave radar quadrotors based on optimal virtual tube
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作者 WU Delong FANG Hao +1 位作者 HAO Yiren WANG Aobo 《Journal of Systems Engineering and Electronics》 2025年第4期1057-1067,共11页
This paper presents a quadcopter system for naviga-tion in outdoor urban environments.The main contributions include the hardware design,the establishment of global occu-pancy grid maps based on millimeter-wave radars... This paper presents a quadcopter system for naviga-tion in outdoor urban environments.The main contributions include the hardware design,the establishment of global occu-pancy grid maps based on millimeter-wave radars,the trajec-tory planning scheme based on optimal virtual tube methods,and the controller structure based on dynamics.The proposed system focuses on utilizing a compact and lightweight quadro-tor with sensors to achieve navigation that conforms to the direction of urban roads with high computational efficiency and safety.Our work is an application of millimeter-wave radars and virtual tube planning for obstacle avoidance in navigation.The validness and effectiveness of the proposed system are verified by experiments. 展开更多
关键词 quadrotor navigation obstacle avoidance millimeter-wave radar virtual tube planning.
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Three-dimension collision-free trajectory planning of UAVs based on ADS-B information in low-altitude urban airspace 被引量:2
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作者 Chao DONG Yifan ZHANG +3 位作者 Ziye JIA Yiyang LIAO Lei ZHANG Qihui WU 《Chinese Journal of Aeronautics》 2025年第2期274-285,共12页
The environment of low-altitude urban airspace is complex and variable due to numerous obstacles,non-cooperative aircraft,and birds.Unmanned Aerial Vehicles(UAVs)leveraging environmental information to achieve three-d... The environment of low-altitude urban airspace is complex and variable due to numerous obstacles,non-cooperative aircraft,and birds.Unmanned Aerial Vehicles(UAVs)leveraging environmental information to achieve three-dimension collision-free trajectory planning is the prerequisite to ensure airspace security.However,the timely information of surrounding situation is difficult to acquire by UAVs,which further brings security risks.As a mature technology leveraged in traditional civil aviation,the Automatic Dependent Surveillance-Broadcast(ADS-B)realizes continuous surveillance of the information of aircraft.Consequently,we leverage ADS-B for surveillance and information broadcasting,and divide the aerial airspace into multiple sub-airspaces to improve flight safety in UAV trajectory planning.In detail,we propose the secure Sub-airSpaces Planning(SSP)algorithm and Particle Swarm Optimization Rapidly-exploring Random Trees(PSO-RRT)algorithm for the UAV trajectory planning in law-altitude airspace.The performance of the proposed algorithm is verified by simulations and the results show that SSP reduces both the maximum number of UAVs in the sub-airspace and the length of the trajectory,and PSO-RRT reduces the cost of UAV trajectory in the sub-airspace. 展开更多
关键词 Three-dimension trajectory planning of UAV Collision avoidance Sliding window ADS-B Low-altitude urban airspace
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Evolution of undeformed chip thickness and grinding forces in grinding of K4002 nickel-based superalloy using corundum abrasive wheels 被引量:1
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作者 Yang CAO Biao ZHAO +6 位作者 Wenfeng DING Xiaofeng JIA Bangfu WU Fei LIU Yanfang ZHU Qi LIU Dongdong XU 《Chinese Journal of Aeronautics》 2025年第1期131-146,共16页
The undeformed chip thickness and grinding force are key parameters for revealing the material removal mechanism in the grinding process.However,they are difficult to be well expressed due to the ununiformed protrusio... The undeformed chip thickness and grinding force are key parameters for revealing the material removal mechanism in the grinding process.However,they are difficult to be well expressed due to the ununiformed protrusion height and random position distribution of abrasive grains on the abrasive wheel surface.This study investigated the distribution of undeformed chip thickness and grinding force considering the non-uniform characteristics of abrasive wheel in the grinding of K4002 nickel-based superalloy.First,a novel grinding force model was established through a kinematic-geometric analysis and a grain-workpiece contact analysis.Then,a series of grinding experiments were conducted for verifying the model.The results indicate that the distribution of undeformed chip thickness is highly consistent with the Gaussian distribution formula.The increase in the grinding depth mainly leads to an increase in the average value of Gaussian distribution.On the contrary,the increase in the workpiece infeed speed or the decrease in the grinding speed mainly increases the standard deviation of Gaussian distribution.The average and maximum errors of the grinding force model are 4.9%and 14.6%respectively,indicating that the model is of high predication accuracy. 展开更多
关键词 K4002 nickel-based superalloy Grinding force Material removal mechanism Undeformed chip thickness Quantity of active abrasive grains
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基于公平性的eVTOL动态合乘匹配与路径规划模型 被引量:1
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作者 任新惠 王孟德 于芳 《北京交通大学学报》 北大核心 2025年第2期58-67,共10页
针对电动垂直起降飞行器(electric Vertical Take-off and Landing,eVTOL)合乘运营场景下的动态请求匹配问题,对合乘匹配及路径规划进行研究.首先,考虑eVTOL垂直起降机场容量、eVTOL载重、电池能耗等限制,以乘客和eVTOL运营商利益最大... 针对电动垂直起降飞行器(electric Vertical Take-off and Landing,eVTOL)合乘运营场景下的动态请求匹配问题,对合乘匹配及路径规划进行研究.首先,考虑eVTOL垂直起降机场容量、eVTOL载重、电池能耗等限制,以乘客和eVTOL运营商利益最大化为目标建立基于合乘公平性的动态eVTOL路径规划模型;其次,使用基本插入算法和线性插入算法对问题模型进行求解,并对比分析按照先到先服务和请求优先级将新请求与eVTOL进行匹配的两种处理方式;最后,以T市5个火车站和1个机场作为垂直机场,用其实际地理位置信息进行算例研究.研究结果表明:与基本插入算法相比,线性插入算法的计算时间缩短了60%以上,证明该算法可以有效求解模型;与按照先到先服务处理方式相比,请求优先级处理新请求时乘客的平均支付费用减少了0.87%,运营商合乘收益提升了5.86%,实现了在保障乘客和运营商利益下新请求与eVTOL的较优匹配.所构建的动态路径规划模型为eVTOL共享运营模式提供参考. 展开更多
关键词 交通运输规划与管理 eVTOL 合乘公平性 请求优先级 线性插入算法
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Clustering optimization strategy for cooperative positioning system aided by UAV 被引量:1
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作者 Hongbo ZHAO Zeqi YIN Shan HU 《Chinese Journal of Aeronautics》 2025年第9期421-435,共15页
For multi-vehicle networks,Cooperative Positioning(CP)technique has become a promising way to enhance vehicle positioning accuracy.Especially,the CP performance could be further improved by introducing Sensor-Rich Veh... For multi-vehicle networks,Cooperative Positioning(CP)technique has become a promising way to enhance vehicle positioning accuracy.Especially,the CP performance could be further improved by introducing Sensor-Rich Vehicles(SRVs)into CP networks,which is called SRV-aided CP.However,the CP system may split into several sub-clusters that cannot be connected with each other in dense urban environments,in which the sub-clusters with few SRVs will suffer from degradation of CP performance.Since Unmanned Aerial Vehicles(UAVs)have been widely used to aid vehicular communications,we intend to utilize UAVs to assist sub-clusters in CP.In this paper,a UAV-aided CP network is constructed to fully utilize information from SRVs.First,the inter-node connection structure among the UAV and vehicles is designed to share available information from SRVs.After that,the clustering optimization strategy is proposed,in which the UAV cooperates with the high-precision sub-cluster to obtain available information from SRVs,and then broadcasts this positioning-related information to other low-precision sub-clusters.Finally,the Locally-Centralized Factor Graph Optimization(LC-FGO)algorithm is designed to fuse positioning information from cooperators.Simulation results indicate that the positioning accuracy of the CP system could be improved by fully utilizing positioning-related information from SRVs. 展开更多
关键词 Clustering optimization Cooperative positioning Locally-centralized FGO Networking wireless sensors Unmanned aerial vehicles Urban degradation environments
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Intelligent sequential multi-impulse collision avoidance method for non-cooperative spacecraft based on an improved search tree algorithm 被引量:1
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作者 Xuyang CAO Xin NING +4 位作者 Zheng WANG Suyi LIU Fei CHENG Wenlong LI Xiaobin LIAN 《Chinese Journal of Aeronautics》 2025年第4期378-393,共16页
The problem of collision avoidance for non-cooperative targets has received significant attention from researchers in recent years.Non-cooperative targets exhibit uncertain states and unpredictable behaviors,making co... The problem of collision avoidance for non-cooperative targets has received significant attention from researchers in recent years.Non-cooperative targets exhibit uncertain states and unpredictable behaviors,making collision avoidance significantly more challenging than that for space debris.Much existing research focuses on the continuous thrust model,whereas the impulsive maneuver model is more appropriate for long-duration and long-distance avoidance missions.Additionally,it is important to minimize the impact on the original mission while avoiding noncooperative targets.On the other hand,the existing avoidance algorithms are computationally complex and time-consuming especially with the limited computing capability of the on-board computer,posing challenges for practical engineering applications.To conquer these difficulties,this paper makes the following key contributions:(A)a turn-based(sequential decision-making)limited-area impulsive collision avoidance model considering the time delay of precision orbit determination is established for the first time;(B)a novel Selection Probability Learning Adaptive Search-depth Search Tree(SPL-ASST)algorithm is proposed for non-cooperative target avoidance,which improves the decision-making efficiency by introducing an adaptive-search-depth mechanism and a neural network into the traditional Monte Carlo Tree Search(MCTS).Numerical simulations confirm the effectiveness and efficiency of the proposed method. 展开更多
关键词 Non-cooperative target Collision avoidance Limited motion area Impulsive maneuver model Search tree algorithm Neural networks
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eVTOL飞行器适坠性研究进展与展望 被引量:1
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作者 刘小川 惠旭龙 +3 位作者 白春玉 李肖成 张欣玥 韩鹤朝 《航空科学技术》 2025年第2期1-28,共28页
电动垂直起降飞行器(eVTOL)作为低空经济领域的新兴装备,具有广阔的应用前景和市场需求,但其安全性尚未得到充分验证和评估,尤其是在紧急情况下的适坠性和乘员保护方面。适坠性是复杂的非线性冲击动力学问题,适航标准和咨询通告等法规... 电动垂直起降飞行器(eVTOL)作为低空经济领域的新兴装备,具有广阔的应用前景和市场需求,但其安全性尚未得到充分验证和评估,尤其是在紧急情况下的适坠性和乘员保护方面。适坠性是复杂的非线性冲击动力学问题,适航标准和咨询通告等法规政策对飞机适坠性作出了明确规定,要求通过合理的设计确保乘客安全,具体涉及机体的坠撞变形与结构吸能、乘员座椅系统的复杂约束与保护措施、起落架系统的吸能设计与承载等多个方面,相关的设计需要通过试验方法或经验证的分析方法进行评估。本文针对eVTOL适坠性研究中的几个关键问题,如适航要求和验证方法、结构适坠性设计、乘员座椅系统坠撞试验与分析、电池系统坠撞试验与分析以及机体结构坠撞试验与分析等近年来的研究情况进行了分析,总结了主要研究进展,并分析了当前研究面临的主要挑战,期望为eVTOL适坠性设计与评估提供一定的借鉴。 展开更多
关键词 eVTOL 适坠性 适航要求 坠撞试验 仿真分析 积木式验证
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SpaceVPX背板交换网络双冗余互连可靠性分析
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作者 吴侃侃 周军 +3 位作者 倪涛 李林伟 张小满 汪少林 《现代电子技术》 北大核心 2025年第8期45-50,共6页
SpaceVPX标准背板控制平面、数据平面双冗余交换网络互连拓扑是实现系统高可靠数据交换的关键。根据SpaceVPX插槽、背板配置规范及可靠性模型分类,建立了一种交换网络可靠性模型,分析了整机双冗余独立备份、交换机互连备份、功能节点交... SpaceVPX标准背板控制平面、数据平面双冗余交换网络互连拓扑是实现系统高可靠数据交换的关键。根据SpaceVPX插槽、背板配置规范及可靠性模型分类,建立了一种交换网络可靠性模型,分析了整机双冗余独立备份、交换机互连备份、功能节点交叉备份、功能节点交叉与交换机互连备份、全连接备份五种拓扑形式的系统可靠性概率。不同拓扑形式的可靠性概率仿真分析结果表明,功能节点交叉备份连接方式适用于控制平面和数据平面双冗余系统。 展开更多
关键词 SpaceVPX 交换网络可靠性模型 控制平面交换 数据平面交换 冗余备份 网络拓扑结构 可靠性概率
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脉冲激光参数对Ti-6Al-4V薄板同轴双激光焊缝成形及其组织性能影响研究
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作者 王红阳 李涛 +2 位作者 尹海鹏 陆连种 刘黎明 《航空制造技术》 北大核心 2025年第14期14-21,共8页
针对钛合金薄板焊接过程中易变形问题,采用由连续激光和脉冲激光组成的同轴双激光器对1.5 mm厚的Ti-6Al-4V薄板进行焊接试验。研究不同激光功率配比、脉宽和频率对焊缝成形和薄板变形的影响,确定了Ti-6Al-4V薄板对焊的最佳焊接工艺参数... 针对钛合金薄板焊接过程中易变形问题,采用由连续激光和脉冲激光组成的同轴双激光器对1.5 mm厚的Ti-6Al-4V薄板进行焊接试验。研究不同激光功率配比、脉宽和频率对焊缝成形和薄板变形的影响,确定了Ti-6Al-4V薄板对焊的最佳焊接工艺参数。试验结果表明,在连续激光功率1.6 kW、脉冲激光功率0.3 kW、脉冲频率25 Hz、脉宽6 ms、焊接速度1000 mm/min的焊接工艺参数下可以获得质量优异的焊缝,变形角度为0.9°。焊接接头抗拉强度为948 MPa,达到母材的92.3%;焊缝表面最大残余压应力为207 MPa,焊缝区和热影响区显微硬度均高于母材。 展开更多
关键词 同轴双激光 TI-6AL-4V 薄板变形 残余应力 组织性能
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eVTOL适坠性分析及优化
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作者 丁梦龙 李道春 +3 位作者 周尧明 冯传宴 邵浩原 向锦武 《航空学报》 北大核心 2025年第11期182-196,共15页
电动垂直起降(eVTOL)飞行器可以在城市内提供便捷的点对点飞行,有望革命性地改变城市居民的出行方式。然而与常规飞机相比,它在耐撞性设计方面存在诸多新挑战。对此,对滑橇式起落架和吸能元件进行了适坠性优化设计,并将其应用于整机适... 电动垂直起降(eVTOL)飞行器可以在城市内提供便捷的点对点飞行,有望革命性地改变城市居民的出行方式。然而与常规飞机相比,它在耐撞性设计方面存在诸多新挑战。对此,对滑橇式起落架和吸能元件进行了适坠性优化设计,并将其应用于整机适坠性分析。同时,开展了多角度、多速度的离轴坠撞仿真研究。鉴于坠撞仿真耗时多、不利于优化设计的问题,提出了使用机器学习技术预测滑橇式起落架应力、吸能元件吸能效率的方法,并且开发了与遗传算法相结合的优化方法。本研究提高了滑橇式起落架、吸能元件、以及eVTOL整机的适坠性能,初步掌握了各离轴坠撞参数对乘员安全的威胁程度,并能在误差可接受范围内实时预测滑橇式起落架应力和吸能元件的吸能效率。 展开更多
关键词 eVTOL 能量吸收 适坠性 机器学习 离轴坠撞
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Distributed predefined-time estimator-based affine formation target-enclosing maneuver control for cooperative underactuated quadrotor UAVs with fault-tolerant capabilities
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作者 Yang XU Yuanfang QU +2 位作者 Delin LUO Haibin DUAN Zhengyu GUO 《Chinese Journal of Aeronautics》 2025年第1期471-490,共20页
The paper presents a two-layer,disturbance-resistant,and fault-tolerant affine formation maneuver control scheme that accomplishes the surrounding of a dynamic target with multiple underactuated Quadrotor Unmanned Aer... The paper presents a two-layer,disturbance-resistant,and fault-tolerant affine formation maneuver control scheme that accomplishes the surrounding of a dynamic target with multiple underactuated Quadrotor Unmanned Aerial Vehicles(QUAVs).This scheme mainly consists of predefinedtime estimators and fixed-time tracking controllers,with a hybrid Laplacian matrix describing the communication among these QUAVs.At the first layer,we devise predefined time estimators for leading and following QUAVs,enabling accurate estimation of desired information.In the second layer,we initially devise a fixed-time hybrid observer to estimate unknown disturbances and actuator faults.Fixedtime translational tracking controllers are then proposed,and the intermediary control input from these controllers is used to extract the desired attitude and angular velocities for the fixed-time rotational tracking controllers.We employ an exact tracking differentiator to handle variables that are challenging to differentiate directly.The paper includes a demonstration of the control system stability through mathematical proof,as well as the presentation of simulation results and comparative simulations. 展开更多
关键词 Affine formation maneuver control Target tracking Fixed-time control Quadrotor unmanned aerial vehicle Target enclosing Predefined-time estimation
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