{"title":"Research on Longitudinal Control Based on UAV Flight Load Test Technology","authors":"Ting Zhu, Lixia Zhao, Jun Yin","doi":"10.1109/icus50048.2020.9274861","DOIUrl":"https://doi.org/10.1109/icus50048.2020.9274861","url":null,"abstract":"Considering that UAV often needs to complete large overload flight in the process of flight load test, it is of great engineering value to study the reachability of large overload target during flight test and overload protection in the full flight envelope. In this paper, based on the longitudinal steep pitch maneuver model in UAV flight load technology, combined with the actual flight control requirements, the response of the aircraft flight attitude parameters when the same overload target is reached in different control time is studied, and the reachability of target overload is evaluated. Based on the UAV stable pitch maneuver model, the simulation obtains the limited boundary of pitch angle rate at different Mach number, indirectly realizes the overload protection in the entire flight envelope and ensures the safety of UAV flight test.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"76 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125492510","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}
{"title":"3DPMNet: Plane Segmentation and Matching for Point Cloud Registration","authors":"Hang Yang, Hui Kong","doi":"10.1109/ICUS50048.2020.9274884","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9274884","url":null,"abstract":"A key task of indoor mobile robot navigation is to register RGB-D frames. Considering that there are many artificial planes in the indoor environment and the matching of planes is more robust than that of points, we propose a new framework to register 3D point clouds with plane correspondences in the scenes. Our framework consists of two parts: a deep neural network titled 3D Plane Matching Net (3DPMNet) which is able to segment and match planes simultaneously by taking raw point clouds as input, and a point-to-plane ICP which utilizes the plane correspondences extracted by 3DPMNet to align the two point clouds. We have generated 22000 point cloud pairs with ground-truth of plane segmentation, plane correspondences and transform matrix from ScanNet. Our experiments demonstrate that the proposed approach performs better than ICP and the recently-proposed learning-based method DCP and PRNet which utilize point correspondences. Moreover, the evaluations on plane segmentation and matching show that our 3DPMNet is able to provide accurate plane correspondences for registration.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121575682","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}
{"title":"Research on the key technology of information communication in unmanned combat system","authors":"Liang Xiaole","doi":"10.1109/ICUS50048.2020.9274997","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9274997","url":null,"abstract":"The unmanned combat system presents the development trend of intelligent perception, functional composition, autonomous control and system coordination, which fundamentally changes the way of human participation in the war. The effectiveness of the unmanned combat system is directly related to the key technology of information communication. Therefore, the paper takes the performance requirements of the information communication in the unmanned combat systems as the start, puts up with building the basic architecture as one network, one database, one platform and one system, adopts advanced frontier information technology and breaks through key technologies such as the information communication transmission, the collaborative communication management and the communication network protection to find countermeasures in order to realize the rapid development of the unmanned combat system of our army.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"27 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126583274","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}
K. Sun, Zichen Fan, Weiran Yao, Yaobing Wang, M. Huo, N. Qi
{"title":"Fast Online Attitude Maneuver Planning of Spacecraft Using Finite Fourier Series Shape-based Method","authors":"K. Sun, Zichen Fan, Weiran Yao, Yaobing Wang, M. Huo, N. Qi","doi":"10.1109/ICUS50048.2020.9275026","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9275026","url":null,"abstract":"In this paper, problem of online fast attitude planning and obstacle avoidance for spacecraft is addressed. A new approach to generate three dimensional trajectory used finite Fourier series (FFS) shape-based method is proposed. By which, time-optimal trajectory under constraints of attitude dynamics and satisfies demand of collision avoidance with obstacles is obtained. Simulation example is set up to validate the effectiveness of the proposed attitude maneuver planning method.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"6 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122336507","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}
{"title":"Continual leakage resilient SM2 signature scheme","authors":"Ding Yujie, Zhang Yingnan, Zhou Tanping","doi":"10.1109/ICUS50048.2020.9274872","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9274872","url":null,"abstract":"Digital signature is a very important primitive in the area of public key cryptography. It guarantees the integrity and irreversibility of the electronic data. Such as the national cryptography SM2 digital signature scheme, which is denoted as SM2 concisely. As everyone knows, there are so many domestic organizations apply SM2 to guarantee the irreversibility and integrity of electronic data, such as Tencent, Ali and the variety of commercial banks. However since the emerging of side-channel attacks which could steal the inner secret information of SM2 during its execution by analyzing running-time, electromagnetic radiation, power consumption, fault detection and many more, the traditional SM2 is no longer secure. For example, once the adversary obtain the secret information such as the secret key used to sign electronic data it can forge any data’s signature. This means that the adversary could steal money and privacy of organizations by forge the corresponding signatures. This is a fatal disease. In this paper we give a continual leakage resilient version of SM2, which aims at achieving that although a part of secret key is continual leaked by side-channel attacks, the adversary couldn’t forge signatures. And then we prove our scheme in the generic bilinear model. Finally, we implement our scheme and test the efficiency which demonstrates the validity and practicability of our scheme.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"38 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116068071","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}
{"title":"M-Estimator Based Robust Coarray Interpolation for DOA Estimation with Miscalibrated Sensors","authors":"Jiaxun Kou, C. Jiang, Ming Li","doi":"10.1109/ICUS50048.2020.9274909","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9274909","url":null,"abstract":"This paper proposes a robust signal interpolation approach for direction-of-arrival (DOA) estimation when several sensors in a coprime array are not properly calibrated. In such case, the conventional interpolation approaches will lead to an inaccurate or even failed DOA estimation. In our proposed approach, observations obtained from the sensors without calibration are blindly treated as outliers. The interpolation problem is formulated as an atomic norm minimization (ANM) problem, where the M-estimator is employed as the regularization term to reduce the adverse impact of outliers. The DOA estimation results can be thus robustly obtained by applying the interpolated virtual signal matrix. Numerical experiments verify that our interpolation algorithm outperformance existing array interpolation methods in terms of robustness.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"10 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123751611","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}
{"title":"Segmented Matching Method of Multi-Geophysics Field SLAM Data Based on LSTM","authors":"Ziyuan Li, Huapeng Yu, Tongsheng Shen, Zhihui Li","doi":"10.1109/ICUS50048.2020.9274964","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9274964","url":null,"abstract":"At present, simultaneous localization and mapping (SLAM) has become an important method for autonomous underwater vehicles (AUVs) to realize long-term navigation. However, using only bathymetric data in unknown environment has its own disadvantages, that are low precision and large computational load. To tackle with requirements of high-precision navigation under large-scale and long-term voyage condition, a SLAM method and corresponding matching algorithm for integrating multi-geophysical field data are proposed. By dividing the feature data and location data of geophysical field obtained into various submaps and sub-segments during AUV sailing, the dominant navigation data of each segment is identified using long short-term memory network. Validity of the proposed method is done by simulation experiments. During the simulation, the loop closure detection of each submap is used, and the matching counter is set to check the correct matching rate. Finally, the matching results with single geophysics field data under the same conditions are compared with multi-geophysics field data and analyzed. The experimental results have demonstrated the feasibility and correctness of the proposed method.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"114 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123865794","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}
{"title":"Static Aeroelastic Effects on Rudder Efficiency of Flying Wing Aircraft","authors":"Cheng Meng, Yuan Kaihua, He Haibo","doi":"10.1109/ICUS50048.2020.9274846","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9274846","url":null,"abstract":"Effects of aeroelastic deformation on control surface efficiency of a flying wing aircraft are investigated using CFD/CSD coupling method. Results indicate that the equivalent deflection angles of inboard elevon, outboard elevon and split rudder decrease due to aeroelastic deformation. As a result, the control surface efficiency is reduced to different degrees. Therefore, in the design of flying wing aircraft, it is necessary to consider the influence of aeroelastic deformation on control surface efficency. Otherwise the control surface efficiency may be insufficient.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"29 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124974365","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}
Chen Junfeng, Li Wuzhou, Wang Yue, Wu Lili, Wu Chao, Xu Fei
{"title":"Flying Qualities Specifications Framework for Unmanned Aircraft Systems based on Mission Task Elements","authors":"Chen Junfeng, Li Wuzhou, Wang Yue, Wu Lili, Wu Chao, Xu Fei","doi":"10.1109/ICUS50048.2020.9274833","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9274833","url":null,"abstract":"Considering the lack of flying qualities specifications of unmanned aircraft systems (UAS), the basic framework of flying qualities specifications based on Mission Task Elements (MTEs) is proposed. Classifications and evaluation objects of UAS in the framework are analyzed by comparing with the characteristics of manned aircraft. As for the construction methods of general framework for UAS flying qualities specification, the three-dimensional classification system, task list descriptions and evaluation methods are discussed. Three-dimensional classification system is proposed based on MTEs, usage and aircraft scale. In addition, task list descriptions are given to explain every task element from classification system. In the aspect of evaluation methods for UAS flying qualities, the objective quantitative evaluation method and subjective criteria evaluation method are discussed. A new modified Cooper-Harper handling qualities rating (HQR) scale for UAS is proposed, which takes the total flight workloads as the index to assess handling qualities, the new workloads proposed synthesize the operator compensation and flight control system (FCS) correction. Furthermore, command response types, airflow effect and pilot induced oscillation (PIO) problems of UAS are discussed, which are investigated by the reference of ADS-33E. This research builds a theoretical foundation and provides a reference for the formulation of flying qualities specifications for UAS.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115179074","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}
{"title":"Overall Technology Research of an UAV-Launcher System Based on Electromagnetic Launch","authors":"Chunyan Liang, Zhiming Qiao, Hong-jun Xiang, Xi-chao Yuan, Xu Zheng, Q. Lv","doi":"10.1109/ICUS50048.2020.9274946","DOIUrl":"https://doi.org/10.1109/ICUS50048.2020.9274946","url":null,"abstract":"Unmanned aerial vehicles (UAVs) have great advantages in maneuverability, economical efficiency, flexible flight and low environmental requirements. While the electromagnetic launch technology has great advantages in controllable launch, accurate armature velocity, clean energy and low recoil. Combining the advantages of the UAV and electromagnetic launch technology, an UAV-Launcher system based on electromagnetic launch is proposed. This article introduces the basic principle, working process and application advantages of that launcher, and key technologies in the UAV-launcher system process are analyzed It provides new ideas for the extended research and innovative application of UAVs and electromagnetic launchers.","PeriodicalId":110715,"journal":{"name":"2020 3rd International Conference on Unmanned Systems (ICUS)","volume":"66 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-11-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122705535","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}