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2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC 2018) Xiamen, China 10 – 12 August 2018 Pages 1-654 IEEE Catalog Number: CFP1829X-POD ISBN: 978-1-5386-1172-2 1/4 Copyright © 2018 by the Institute of Electrical and Electronics Engineers, Inc. All Rights Reserved Copyright and Reprint Permissions: Abstracting is permitted with credit to the source. Libraries are permitted to photocopy beyond the limit of U.S. copyright law for private use of patrons those articles in this volume that carry a code at the bottom of the first page, provided the per-copy fee indicated in the code is paid through Copyright Clearance Center, 222 Rosewood Drive, Danvers, MA 01923. For other copying, reprint or republication permission, write to IEEE Copyrights Manager, IEEE Service Center, 445 Hoes Lane, Piscataway, NJ 08854. All rights reserved. *** This is a print representation of what appears in the IEEE Digital Library. Some format issues inherent in the e-media version may also appear in this print version. IEEE Catalog Number: CFP1829X-POD ISBN (Print-On-Demand): 978-1-5386-1172-2 ISBN (Online): 978-1-5386-1171-5 Additional Copies of This Publication Are Available From: Curran Associates, Inc 57 Morehouse Lane Red Hook, NY 12571 USA Phone: (845) 758-0400 Fax: (845) 758-2633 E-mail: [email protected] Web: www.proceedings.com TABLE OF CONTENTS STUDY ON LOW ENERGY MOON RETURN ORBIT CONSTRUCTION AND LOW THRUST PROPULSION CONTROL STRATEGY ........................................................................................................................... 1 Yue Liu ; Yingjing Qian ; Wuxing Jing EVOLVEMENT LAWS OF MAGNETIC DIPOLES INTERACTION AND ITS APPLICATION TO SPACECRAFT SELF- AND SOFT-DOCKING* ............................................................................................................... 7 Yuan-Wen Zhang ; Le-Ping Yang ; Yan-Wei Zhu ; Huan Huang ; Da-Wei Qi ; Jin-Liang Jie GUST LOAD ALLEVIATION OF AIRCRAFT WITH MULTIPLE CONTROL EFFECTORS IN THE CRUISE PHASE BASED ON L1 ADAPTIVE NONLINEAR DYNAMIC INVERSION AND CONTROL ALLOCATION ............................................................................................................................................... 13 Jinglong Liu ; Weiguo Zhang ; Xiaoxiong Liu ; Yunxiao Qin MULTI-ROTOR UAVS FORMATION CONTROL AND AVOIDANCE TECHNOLOGY BASED ON AD-HOC NETWORK STRATEGY ........................................................................................................................... 21 Yu Zheng ; Zhihao Cai ; Jiang Zhao ; Yingxun Wang ; Xuedong Zhao ; Dongliang Song OPTIMAL COLLISION AVOIDANCE UNDER THE VELOCITY UNCERTAINTY IN LEO ................................ 28 Bing Hua ; Yu Huang ; Zhenxing Li ; Yunhua Wu ; Zhiming Chen SIMULATION OF UNMANNED AIRCRAFT SYSTEM PERFORMING SURVEILLANCE MISSION BASED ON ADVANCED DISTRIBUTED ARCHITECTURE .................................................................... 34 Hongxia Ji ; Peng Yao ; Honglun Wang ; Jianfa Wu IMPROVE PID CONTROLLER THROUGH REINFORCEMENT LEARNING ....................................................... 38 Yunxiao Qin ; Weiguo Zhang ; Jingping Shi ; Jinglong Liu ROBUST STABILIZATION CONTROL FOR ATTITUDE ANGULAR SPEEDS OF STRONG- COUPLING AIRCRAFT BASED ON A CLASS OF ESO .............................................................................................. 44 Xiaodong Liu ; Yuteng Cao ; Yu Zhang ; Yong Min ; Zhiqiang Jia ON ACTIVE SIDESTICK FORCE CONTROL STRATEGY TECHNOLOGY * ....................................................... 50 Huang Zilinu ; Lu Zhengren FDI AND NAVIGATION INTEGRATION ALGORITHM DESIGN FOR SKEW REDUNDANT STRAPDOWN INERTIAL MEASUREMENT UNIT ..................................................................................................... 55 Weizheng Zhou ; Xuefeng Li ; Saijun Zhao ; Jiansheng Tao METHOD FOR TARGET GROUPING BASED ON CFSFDP ALGORITHM ............................................................ 60 Li Weinan ; Zhang Weiguo ; Shi Jingping ; Wu Yunyan A RESEARCH ON THE SHORT-TAKEOFF PERFORMANCE AND FLIGHT CONTROL OF STOVL AIRCRAFT ............................................................................................................................................................ 66 Kun Chen ; Junquan Fu ; Jiachen Zhu IMPACT OF EPHEMERIS ERRORS ON X-RAY PULSAR NAVIGATION .............................................................. 72 Q. Xu ; H. L. W ; S. H. You ; Y. Y. He ; L. Feng ON DYNAMIC LOGARITHMIC QUANTIZER DESIGN FOR CONTINUOUS TIME LINEAR SYSTEMS ............................................................................................................................................................................. 78 Jiashuo Wang ; Zhiyu Xi ROBUST CENTRALIZED FUSION TIME-VARYING KALMAN FILTERS ............................................................ 84 Wenjuan Qi ; Zunbing Sheng ; Cong Shen MULTI-UAVS TARGET TRACKING IN URBAN ENVIRONMENT BASED ON DISTRIBUTED MODEL PREDICTIVE CONTROL AND LEVY FLIGHT-SALP SWARM ALGORITHM ..................................... 88 Menghua Zhang ; Honglun Wang ; Jianfa Wu DESIGN OF A NOVEL UNIAXIAL TUNNELING MAGNETORESISTANCE ACCELEROMETER .................... 94 Binlong Wang ; Bo Yang ; Chengfu Lu REDUCED-ORDER LINEAR EXTENDED STATE OBSERVER BASED TRAJECTORY LINEARIZATION CONTROL FOR HYPERSONIC REENTRY VEHICLE UNDER HIGH MANEUVER FLIGHT WITH MULTIPLE DISTURBANCES ..................................................................................... 98 Huiping Zhang ; Yue Yu ; Honglun Wang ; Yiheng Liu A NONLINEAR ADAPTIVE CONTROL METHOD AND ITS APPLICATION TO A WIND TUNNEL SYSTEM ........................................................................................................................................................... 104 Bi Zhang ; Xin-Gang Zhao ; Ting-Feng Zhang ; Feng Yu THE DESIGN OF STORES MANAGEMENT SYSTEM SIMULATOR BASED ON PLUG-IN TECHNOLOGY ................................................................................................................................................................ 109 Li Jia-Hui ; Chen Shao-Dong ; Chen Xiao-Yang EFFECT ANALYSIS OF MISSILE DECOY DISTRIBUTION ON EXO-ATMOSPHERE KINETIC INTERCEPTOR ................................................................................................................................................................ 114 Taotao Zhang ; Haoyu Wang ; Sen Shen ; Nianxuan Li ; Wei Jiang DYNAMIC SURFACE FUZZY ADAPTIVE TERMINAL GUIDANCE LAW WITH IMPACT ANGLE CONSTRAINTS AND AUTOPILOT LAG ...................................................................................................... 118 Jiang Shang ; Liang Weige ; Tian Fuqing ; Sun Shiyan OPTIMIZATION OF COOPERATIVE DEPLOYMENT OF MULTIPLE TERMINAL DEFENSE SYSTEM ............................................................................................................................................................................. 124 Jian Li ; Shunhong Wang ; Chenchao Dai ; Qinhong Tang ; Xiaoqiang Tian INTEGRATED GUIDANCE AND CONTROL FOR UAV STANDOFF TARGET TRACKING ............................ 130 Shanshan Cheng ; Dawei Li ; Na Li ; Honglun Wang ; Jianfa Wu ; Zikang Su ; Menghua Zhang COOPERATIVE GUIDANCE AGAINST STATIONARY AND NON-MANEUVERING TARGETS .................... 136 Jianbo Zhao ; Shuxing Yang ; Fenfen Xiong REAL-TIME MOTION PLANNING FOR QUADROTOR MAVS IN THREE-DIMENSIONAL COMPLEX ENVIRONMENT ......................................................................................................................................... 142 Zhengda Zhu ; Nong Cheng ; Qing Li TAXIING CONTROL OF FULL-WING SOLAR-POWERED UAV BY USING DIFFERENTIAL PROPELLER THRUST .................................................................................................................................................... 148 Ma Zhenyu ; Zhu Xiaoping ; Zhou Zhou SCHROEDER PHASED HARMONIC SIGNAL APPLIED IN FREQUENCY RESPONSE TEST OF MISSILE STEERING GEAR SYSTEM .......................................................................................................................... 153 Changpeng Su ; Xuemei Wang ; Zhe Xu ; Jianyong Wang ; Junxiao Li ; Hongbin Qiu ; Xinglong Wang CROSS-MEDIUM ATTITUDE CONTROL OF SUBMARINE-TO-AIR MISSILE BASED ON IMPLICIT INCREMENTAL SLIDING-MODE ............................................................................................................ 158 Miao Haochun ; Ma Qinghua ; Wang Gen ; Chen Yun A COMBINED VISUAL-INERTIAL NAVIGATION SYSTEM OF MSCKF AND EKF-SLAM ............................. 162 Jian Li ; Qing Li ; Nong Cheng MATRIX COMPLETION BASED AEROENGINE ANALYTICAL REDUNDANCY ............................................. 168 Zepeng Lu ; Nong Cheng ; Qing Li A NEW THREE-DIMENSIONAL TRACKING GUIDANCE BASED ON FULL STATE COUPLING* ...................................................................................................................................................................... 173 A. Yuan-Long Zhang ; B. Rui-Zhi He ; C. Kai-Chuan Xu ; D. Guo-Jian Tang ; E. Wei-Min Bao IDENTIFICATION OF SURGE INCEPTION IN AERO-ENGINE COMPRESSOR USING S- TRANSFORM .................................................................................................................................................................... 179 Danni Yu ; Nong Cheng ; Qing Li ; Binhe Wen GENETIC ALGORITHM-PARTICLE SWARM OPTIMIZATION ALGORITHM BASED COMPASS INITIAL ALIGNMENT OF STRAPDOWN INERTIAL NAVIGATION SYSTEM ............................. 184 Jiang Peng-Fei ; Xu Jiang-Ning ; Zhu Bing REGRESS ANALYSIS FILTERING ALGORITHM
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