2013 International Conference on Unmanned Aircraft Systems (ICUAS)最新文献

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Statistical methods and weather based decision making in meteorological support for unmanned aerial vehicles (UAVs) 无人机气象保障中的统计方法和基于天气的决策
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564691
F. Wantuch, Z. Bottyán, Z. Tuba, K. Hadobács
{"title":"Statistical methods and weather based decision making in meteorological support for unmanned aerial vehicles (UAVs)","authors":"F. Wantuch, Z. Bottyán, Z. Tuba, K. Hadobács","doi":"10.1109/ICUAS.2013.6564691","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564691","url":null,"abstract":"Two different methods had been developed to support special UAV applications reducing the weather risk during flights. In our study we explain the analogue method based on climate statistics was applied for the estimation of occurrence of different weather phenomena. As we show the analog weather situations can play an important role in the weather prediction for the UAVs, too. With the help of a case study we demonstrate the usefulness of this method in the visibility prediction. On the other hand in order to determine the optimal UAV flight path an optimal graph theoretical approach had been applied. Described procedures are also illustrated with examples in our present work.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"18 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127915599","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 5
Platform design and mathematical modeling of an ultralight quadrotor micro aerial vehicle 超轻型四旋翼微型飞行器平台设计与数学建模
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564797
Kun Li, S. K. Phang, Ben M. Chen, Tong-heng Lee
{"title":"Platform design and mathematical modeling of an ultralight quadrotor micro aerial vehicle","authors":"Kun Li, S. K. Phang, Ben M. Chen, Tong-heng Lee","doi":"10.1109/ICUAS.2013.6564797","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564797","url":null,"abstract":"In this paper, a micro quadrotor aircraft with approximately 40 g gross weight and 8 min flight endurance is developed. System development of this micro aerial vehicle is discussed in terms of the design of the mechanical structure and electrical systems. Mechanical structure is designed based on the proposed weight budget, propulsion system efficiency as well as results of structural analysis. Mechanical parts are designed and analyzed with 3D simulation software then 3D printed. Development of the electrical systems includes integration of processor, inertia measurement unit, and communications with commercial off-the-shelf electronics. Finally, a mathematical model of the quadrotor is derived based on the quadrotor X-configuration working principle. Parameters involved are further identified with experimental setups or simulations. The controller is first simulated with software simulator and then tuned with real flight tests.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127935129","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 15
On the maneuverability of small unmanned aerial vehicles 小型无人机机动性能研究
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564677
F. D. de Almeida, J. P. C. Escosteguy, F. A. D'Oliveira
{"title":"On the maneuverability of small unmanned aerial vehicles","authors":"F. D. de Almeida, J. P. C. Escosteguy, F. A. D'Oliveira","doi":"10.1109/ICUAS.2013.6564677","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564677","url":null,"abstract":"Collision avoidance is a key issue in the current effort to allow Unmanned Aerial Systems (UAS) operations in non-segregated airspace. Several Sense and Avoid technologies are being studied, and should be available in the near future. Surprisingly, there are few references in the literature dealing with another important factor: the ability of UAS to perform the necessary avoidance maneuvers. This work discusses the maneuverability of small unmanned aerial vehicles, based on important factors as wing loading and thrust to weight ratio, which influence the minimum and maximum attainable values of airspeed, climb angle and turning rate. The polyhedral flight envelopes of two versions of a small aerial vehicle are constructed to allow better visualization of the influence of aircraft design parameters and also the impact of some commonly adopted operational procedures of autonomous aerial systems.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126581270","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
Robust Fault Estimation on a real quadrotor UAV using optimized Adaptive Thau Observer 基于优化自适应Thau观测器的四旋翼无人机鲁棒故障估计
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564732
Zhaohui Cen, H. Noura, Younes Al Younes
{"title":"Robust Fault Estimation on a real quadrotor UAV using optimized Adaptive Thau Observer","authors":"Zhaohui Cen, H. Noura, Younes Al Younes","doi":"10.1109/ICUAS.2013.6564732","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564732","url":null,"abstract":"As a result of modeling uncertainties, data decade unbalanceand noise, Fault Estimation (FE) for real quadrotor is rough with low accuracy when model observer based FE scheme-Adaptive Thau Observer(ATO) is applied. Based on these issues, this paper proposes a comprehensive optimization approach on FE accuracy for quadrotor using ATO. First, the ATO observer is improved by adding unmolded terms with parameters derived from identification. Secondly, a data adjustment based on amplifying and reducing is introduced to overcome the data decade unbalance. Thirdly, the Infinite Impulse Response (IIR) filter is utilized to decrease the noise in measurement signals. Finally, experiments for injecting the rotor fault have been carried out to show the effectiveness of the proposed optimization method and the results are discussed.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122232147","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 16
3D path planning for UAVs for maximum information collection 无人机三维路径规划,最大限度地收集信息
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564676
H. Ergezer, M. Leblebicioğlu
{"title":"3D path planning for UAVs for maximum information collection","authors":"H. Ergezer, M. Leblebicioğlu","doi":"10.1109/ICUAS.2013.6564676","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564676","url":null,"abstract":"This paper addresses the problem of path planning for multiple UAVs. The paths are planned to maximize collected amount of information from Desired Regions (DR) while avoiding Forbidden Regions (FR) violation and reaching the destination. The approach extends prior study for multiple UAVs by considering 3D environment constraints. The path planning problem is studied as an optimization problem. The problem has been solved by a Genetic Algorithm (GA) with the proposal of novel evolutionary operators. The initial populations have been generated from a seed-path for each UAV. The seed-paths have been obtained both by utilizing the Pattern Search method and solving the multiple-Traveling Salesman Problem (mTSP). Utilizing the mTSP solves both the visiting sequences of DRs and the assignment problem of \"which DR should be visited by which UAV\". It should be emphasized that all of the paths in population in any generation of the GA have been constructed using the dynamical mathematical model of an UAV equipped with the autopilot and guidance algorithms. Simulations are realized in the MATLAB/Simulink environment. The path planning algorithm has been tested with different scenarios, and the results are presented in Section V. Although there are previous studies in this field, this paper focuses on maximizing the collected information instead of minimizing the total mission time. Even though, a direct comparison of our results with those in the literature is not possible, it has been observed that the proposed methodology generates satisfactory and intuitively expected solutions.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"31 9","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114086272","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 18
Modeling multiple unmanned aerial vehicles placement problem in ad hoc network via quadratic unconstrained binary optimization 基于二次型无约束二元优化的自组网多无人机布局问题建模
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564778
Haibo Wang, Wei Wang, Jun Huang, Da Huo, Yaquan Xu
{"title":"Modeling multiple unmanned aerial vehicles placement problem in ad hoc network via quadratic unconstrained binary optimization","authors":"Haibo Wang, Wei Wang, Jun Huang, Da Huo, Yaquan Xu","doi":"10.1109/ICUAS.2013.6564778","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564778","url":null,"abstract":"This paper addresses an important issue in ad hoc network connectivity using unmanned aerial vehicles (UAVs) as relay nodes and formulates the problem of locating UAVs in the network as a facility location problem. We propose a method to reformulate the facility location problem using quadratic unconstrained binary optimization (QUBO) and solve the QUBO model with off-shelf software. The analysis of the solutions produced by QUBO along with comparisons made with the linear model highlights both the attractiveness and robustness of the proposed approach.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"38 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124944292","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 9
Coverage control in multi-vehicle systems subject to health degradation 受健康退化影响的多车辆系统的覆盖控制
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564802
F. Sharifi, Youmin Zhang, A. Aghdam
{"title":"Coverage control in multi-vehicle systems subject to health degradation","authors":"F. Sharifi, Youmin Zhang, A. Aghdam","doi":"10.1109/ICUAS.2013.6564802","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564802","url":null,"abstract":"This paper presents a distributed deployment algorithm for a network of multi-vehicle systems to minimize a prescribed cost function. The goal is to perform a coverage task when the capability of the vehicles to carry out the task varies through time. The problem is investigated for the case where vehicles have variable sensing performance. A specific partitioning technique is used to address this problem, and optimal configuration for vehicles is also introduced. A distributed coverage control is then provided which guarantees the convergence of vehicles to the best configuration subject to health degradation due to faults in individual vehicle of the team. The effectiveness of the proposed algorithms is demonstrated by numerical simulations.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"30 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126981827","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 5
Real-time altitude robust controller for a Quad-rotor aircraft using Sliding-mode control technique 基于滑模控制技术的四旋翼飞行器实时高度鲁棒控制器
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564745
I. González, S. Salazar, R. Lozano, J. Escareño
{"title":"Real-time altitude robust controller for a Quad-rotor aircraft using Sliding-mode control technique","authors":"I. González, S. Salazar, R. Lozano, J. Escareño","doi":"10.1109/ICUAS.2013.6564745","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564745","url":null,"abstract":"A real-time robust altitude control scheme is proposed for the efficient performance of a Quadrotor aircraft system. The sensing of altitude measurement sensing is performed by a pressure sensor in order to obtain a robust altitude control of the vehicle in hovering mode both indoor and outdoor. The altitude measurement has the advantage of introducing this state information directly in the closed loop control which should be very useful for achieving robust stabilization of the altitude of the vehicle. To this end, a Sliding Mode Control strategy is implemented for the Quad-rotor aircraft. We have assumed that the actuators are able to respond quickly and accurately and we have not enforced limits on the control signals. Finally, to verify the satisfactory performance of proposed nonlinear control law, simulations and experimental results of the Sliding Mode Control technique for the Quadrotor aircraft in the presence of bounded disturbances are presented.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"55 4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127595298","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 14
Development of a complex dynamical modeling system for the meteorological support of unmanned aerial operation in Hungary 开发一个复杂的动态建模系统,为匈牙利的无人机操作提供气象支持
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564668
A. Z. Gyongyosi, P. Kardos, Rita Kurunczi, Z. Bottyán
{"title":"Development of a complex dynamical modeling system for the meteorological support of unmanned aerial operation in Hungary","authors":"A. Z. Gyongyosi, P. Kardos, Rita Kurunczi, Z. Bottyán","doi":"10.1109/ICUAS.2013.6564668","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564668","url":null,"abstract":"Proper, detailed and specific meteorological information is essential in aviation meteorology and may be especially critical in unmanned aerial operations. The aim of the research partially described in the present paper is the development of a weather prediction system that is suitable for the above purpose. The dynamical modeling component of the system was tailored and tested for the special needs of aviation weather forecasting for unmanned aerial operations in the Carpathian basin. Following an extensive technical implementation, the so-called Weather Research and Forecasting limited area model has been applied for this purpose. The applicability of the model system have been investigated on 9 typical weather situations, all of them having aeronautical safety relevance from the weather hazard point of view, all of the selected test case type weather situations are having significant influence on the weather of Hungary. The fine tuning of the model setup included parallel run of 30 different setup model versions, as ensemble members, each of them having different combination of parameterization. Verification of the ensemble members against observation yielded the optimal model version for the present purpose. Furthermore, meteorological measurements with sensors installed on UAV platform have been done. Following the short introduction of the weather prediction system that was applied, results of the case study test runs are compared to observation. The experiences of the first UAV flights are also presented. Results are introduced and the directions towards further development are described.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"47 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134030626","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 7
Adaptive fault-tolerant control design for UAVs formation flight under actuator faults 执行器故障下无人机编队飞行自适应容错控制设计
2013 International Conference on Unmanned Aircraft Systems (ICUAS) Pub Date : 2013-05-28 DOI: 10.1109/ICUAS.2013.6564799
Qing Xu, Hao Yang, B. Jiang, Donghua Zhou, Youmin Zhang
{"title":"Adaptive fault-tolerant control design for UAVs formation flight under actuator faults","authors":"Qing Xu, Hao Yang, B. Jiang, Donghua Zhou, Youmin Zhang","doi":"10.1109/ICUAS.2013.6564799","DOIUrl":"https://doi.org/10.1109/ICUAS.2013.6564799","url":null,"abstract":"This paper studies fault tolerant control(FTC) method of incipient and severe actuator faults of unmanned aerial vehicles (UAVs) formation. We first design a feedback control for the initial normal system. In the event of actuator faults, a compensation is add into the initial controller to accomplish fault tolerant and stabilize the whole formation as well. Then the difference between controllers of incipient and severe faults is analyzed. Finally the proposed method is illustrated via 5-UAV formation example.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"276 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124446734","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 4
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