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2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)最新文献

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Spacecraft attitude control using nonsingular finite-time convergence Terminal Sliding Mode 基于非奇异有限时间收敛终端滑模的航天器姿态控制
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7828857
Z. Han, Ke Zhang, Tianshe Yang
{"title":"Spacecraft attitude control using nonsingular finite-time convergence Terminal Sliding Mode","authors":"Z. Han, Ke Zhang, Tianshe Yang","doi":"10.1109/CGNCC.2016.7828857","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7828857","url":null,"abstract":"Finite-time convergence control strategies based on adaptive Nonsingular Terminal Sliding Mode are proposed for spacecraft attitude tracking control subject to external disturbances and actuator faults. The designed attitude tracking controller meets the multi-constraints, and has singularities avoidance attributes. It is further shown that the controller with parameter adaptations is independent from bound of external disturbances. The Lyapunov stability analysis shows that the controller designed in this paper can guarantee the fast convergence of the closed-loop system, and has a good fault tolerant performance on actuator faults under the multi-constraints on external disturbances and actuator faults. Numerical simulation verified the good performance of the controller in the attitude tracking control.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"60 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126985363","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: 6
Magnetic-based Attitude Control scheme for CubeSat 基于磁力的立方体卫星姿态控制方案
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7828771
Xiwang Xia, Shufan Wu, Guowen Sun, Tian-Zhe Wang, Ziyi Wu, Yanping Bai, Wen Chen, Z. Mu
{"title":"Magnetic-based Attitude Control scheme for CubeSat","authors":"Xiwang Xia, Shufan Wu, Guowen Sun, Tian-Zhe Wang, Ziyi Wu, Yanping Bai, Wen Chen, Z. Mu","doi":"10.1109/CGNCC.2016.7828771","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7828771","url":null,"abstract":"Nowadays, the development of low-cost CubeSats is very active. As the cheapest satellites are commonly used to demonstrate some novel technologies and dedicated to science researches, the requirements of Attitude Determination and Control System (ADCS) have been not very severe. Magnetic-based attitude control scheme is widely adopted by CubeSats for damping and stabilizing with several magnetic torquers employed. STTJ-2A, developed by Shanghai Engineering Center for Microsatellites, adopts such scheme with 3 reaction wheels equipped. However, the magnetic-based attitude control scheme, employing three magnetic torquers with or without a biased momentum wheel, is the basic attitude control strategy. Once being ejected into the orbit, the satellite would employ magnetic torquers to damp itself, and then, be controlled to Sun-pointing or Nadir-pointing. After the wheel is started up, rotation of the wheel would provide gyroscopic stiffness, while the attitude would still be controlled by the magnetic torquers. During the design of the corresponding attitude control laws, Quasi-Euler Angles, which are derived from quaternions and have similar characteristics with the classic Euler angles, are adopted to describe the attitude. Simulation results indicate that the designed attitude control schemes are effective and the pointing accuracy corresponding to nadir-pointing mode and biased-momentum mode are 15deg and 3deg respectively.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"12 8","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"120852328","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: 12
Research on relative navigation algorithm for UAV Autonomous Aerial Refueling rendezvous phase 无人机自主空中加油交会阶段相关导航算法研究
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7829111
Zhu Yunfeng, Sun Yongrong, Huang Bin, Lin Rongbing, Wu Ling
{"title":"Research on relative navigation algorithm for UAV Autonomous Aerial Refueling rendezvous phase","authors":"Zhu Yunfeng, Sun Yongrong, Huang Bin, Lin Rongbing, Wu Ling","doi":"10.1109/CGNCC.2016.7829111","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7829111","url":null,"abstract":"The lack of Autonomous Aerial Refueling capability is one of the greatest limitations of UAV (unmanned aerial vehicle). The estimation of the relative position, velocity and attitude is the key issue in this research area. This paper proposes a novel method for relative navigation. We focus on the need for the rendezvous phase. The structure of this paper is as follows. Firstly, we shall briefly introduce the autonomous aerial refueling phases and the related navigation sensors. Then we establish the error equation. After using the Kalman filter, we obtain the estimation of the relative state error. The employed algorithm based on the SINS/GPS/IRST integrated relative navigation, it has advantages of both autonomous navigation and passive target positioning. In simulation experiments, the results show that our algorithm can track the relative state variation and restrain the error divergency effectively.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"26 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114742436","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: 3
Fault detection based on Sensitive Marginal Fisher Analysis for class imbalance 基于敏感边际Fisher分析的类不平衡故障检测
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7828774
Zhiyan Han, Jian Wang
{"title":"Fault detection based on Sensitive Marginal Fisher Analysis for class imbalance","authors":"Zhiyan Han, Jian Wang","doi":"10.1109/CGNCC.2016.7828774","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7828774","url":null,"abstract":"The class imbalance problem has made researchers pay intensive attention in recent years. In the modern semiconductor industry, the class imbalance makes fault detection, which aims at constructing a decision tool to maintain high process yields, quite challenging. Marginal Fisher Analysis (MFA) is a popular method which can analyze the discriminant relationship between data points from different classes, and has been applied in fault detection. However, the performance of MFA is poor if it is applied in the data having imbalance distributing between classes. This paper analyzes the challenge of class imbalance and a improved approach of MFA named Sensitive Margin Fisher Analysis (SMFA) was proposed for the problem. The proposed fault detection method has been verified by applying it in the semiconductor wafer fabrication process. The experiment results confirm the new method improves the fault detection performance.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"116 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124137010","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: 3
A survey on concurrent network localization for autonomous multi-vehicle systems 自主多车系统并行网络定位研究
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7828994
Tingrui Han, Zhiyun Lin, Ronghao Zheng
{"title":"A survey on concurrent network localization for autonomous multi-vehicle systems","authors":"Tingrui Han, Zhiyun Lin, Ronghao Zheng","doi":"10.1109/CGNCC.2016.7828994","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7828994","url":null,"abstract":"Network localization plays the key role in position based operations and services of autonomous multi-vehicle systems such as unmanned aerial vehicles and satellite formation, which aims to determine the Euclidean coordinates of all the vehicles given a collection of inter-vehicle measurements and the Euclidean coordinates of a small number of vehicles. Concurrent network localization approaches allow each vehicle solve its own coordinate in a distributed manner via local information exchange with its neighbors and thus exhibit many desirable advantages in applications. This paper reviews recent development on concurrent network localization algorithms and aims to provide a comprehensive insight for these novel ideas. In terms of the types of inter-vehicle information, distance-based, bearing-based, and relative-position-based concurrent network localization are discussed in a unified framework.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128064688","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: 0
Protein secondary structure prediction via Pigeon-Inspired Optimization 基于鸽子启发优化的蛋白质二级结构预测
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7829085
Wei Zheng, Hemeng Sun, H. Duan
{"title":"Protein secondary structure prediction via Pigeon-Inspired Optimization","authors":"Wei Zheng, Hemeng Sun, H. Duan","doi":"10.1109/CGNCC.2016.7829085","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7829085","url":null,"abstract":"Proteins are the essential elements in all creatures' life process. The prevailing experimental method to detect protein structure is time consuming. According to Anfinsen's theory, the primary structure is the key to shaping the three-dimensional structure of the protein. Thus, the prediction of proteins' structure avoiding complex experiments is theoretically feasible. Algorithms are applied to make the protein structure prediction while they have some unsatisfactory blemish. For instance, relatively high Gibbs free energy or long iterating progress. In this paper, a new algorithm is introduced to solve this problem. Its name is “Pigeon-Inspired Optimization(PIO) Algorithm”. PIO can work out an accurate prediction in relatively short iterations. The advantages and feasibility of this algorithm will be demonstrated through the experiments, comparing to Particle Swarm Optimization.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"33 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127877295","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: 3
Carrier-based aircraft ski-jump take-off control system and visual simulation 舰载机滑跃起飞控制系统及视觉仿真
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7828983
Liuqing Yang, Z. Zhen, Kangwei Li, Chunye Jia
{"title":"Carrier-based aircraft ski-jump take-off control system and visual simulation","authors":"Liuqing Yang, Z. Zhen, Kangwei Li, Chunye Jia","doi":"10.1109/CGNCC.2016.7828983","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7828983","url":null,"abstract":"This paper addresses the ski-jump take-off control problem of the carrier-based aircraft. A nonlinear model of the carrier-based aircraft is established. PID control method is used to design the longitudinal controllers and the lateral controllers of the ski-jump take-off control system. The longitudinal controllers include the vertical speed controller, longitudinal stabilization system and velocity controller. The lateral controllers include the roll angle controller, yaw angle controller and lateral deviation controller. The influence of the flight deck movement on the take-off process is investigated. The ski-jump take-off process is simulated by Matlab/Simulink and the take-off flight control system is verified. Three dimensional visual simulation is carried out to improve the demonstration effect of the ski-jump take-off process.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"97 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115842902","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
Robust adaptive tracking control for uncertain nonlinear systems with external disturbances 不确定非线性系统的鲁棒自适应跟踪控制
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7829025
Yashun Zhang, Hui Wang, Chao Yang
{"title":"Robust adaptive tracking control for uncertain nonlinear systems with external disturbances","authors":"Yashun Zhang, Hui Wang, Chao Yang","doi":"10.1109/CGNCC.2016.7829025","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7829025","url":null,"abstract":"This paper is concerned with the tracking control problem for nonlinear systems with unknown time-varying parameter uncertainties and unknown external disturbances. The problem addressed is to design robust adaptive controllers that guarantee the tracking of a given reference signal. A robust adaptive control scheme is firstly proposed for the case the external disturbance is square-integrable. Then the design scheme is extend to the asymptotically tracking control of the nonlinear system with bounded disturbances. Finally, the effectiveness of the proposed design method is demonstrated by an application example.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"31 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115924064","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: 0
Chattering free sliding adaptive attitude control for quadrotor 四旋翼飞行器颤振自由滑动自适应姿态控制
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7828872
Zhi Li, Xin Ma, Zhigang Xu, Yafang Wang, Yibin Li
{"title":"Chattering free sliding adaptive attitude control for quadrotor","authors":"Zhi Li, Xin Ma, Zhigang Xu, Yafang Wang, Yibin Li","doi":"10.1109/CGNCC.2016.7828872","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7828872","url":null,"abstract":"This paper investigates the quadrotor attitude tracking control problem in the presence of external disturbance and inertia uncertainty. An error quaternion based adaptive sliding mode control scheme is proposed in this paper. Adaptive control theory is applied to estimate inertia parameters and the upper bound of external disturbance. Lyapunov stability theory is applied to prove the stability of the controller. Simulation results are presented to demonstrate the performance and robustness of the controller.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"22 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132049254","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
A dynamic error excitation and calibration method for high precision IMU 高精度IMU的动态误差激励与标定方法
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) Pub Date : 2016-08-01 DOI: 10.1109/CGNCC.2016.7829024
Li Xing, Qingqing Bai, Zhi Xiong, Wei Luo, Jianye Liu
{"title":"A dynamic error excitation and calibration method for high precision IMU","authors":"Li Xing, Qingqing Bai, Zhi Xiong, Wei Luo, Jianye Liu","doi":"10.1109/CGNCC.2016.7829024","DOIUrl":"https://doi.org/10.1109/CGNCC.2016.7829024","url":null,"abstract":"According to the urgent need of high-precision navigation system to future fighters, this paper researches on a dynamic error excitation and calibration method for high-precision IMU. The Kalman filter model including installation errors, scale factor errors and random constant errors of the inertial measurement unit (IMU) as state variables for online identification is established. The relationship between IMU errors and aircraft maneuver manner is derived, and the dynamic flight track to incite IMU errors is designed. Simulation results verify the feasibility of the proposed dynamic error parameter excitation and calibration method, which can incite and identify the IMU error effectively. With the error identification results, the IMU errors are compensated and the precision of the INS is improved significantly.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130143241","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: 0
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