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    IEEE Chinese Guidance, Navigation and Control Conference (CGNCC), 2014 : 8 - 10 Aug. 2014, Yantai, China

    Institute of Electrical and Electronics Engineers | TIBKAT | 2014
    Publisher: IEEE , Piscataway, NJ
    Keywords: Navigation (Aeronautics)

    2014 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC 2014) : Yantai, China, 8 - 10 August 2014 ; 1

    Institute of Electrical and Electronics Engineers | TIBKAT | 2014
    Publisher: IEEE , Piscataway, NJ

    2014 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC 2014) : Yantai, China, 8 - 10 August 2014 ; 3

    Institute of Electrical and Electronics Engineers | TIBKAT | 2014
    Publisher: IEEE , Piscataway, NJ

    2014 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC 2014) : Yantai, China, 8 - 10 August 2014 ; 2

    Institute of Electrical and Electronics Engineers | TIBKAT | 2014
    Publisher: IEEE , Piscataway, NJ

    2016 IEEE Chinese Guidance, Navigation and Control Conference : IEEE CGNCC 2016 : August 12-14, 2016, Nanjing, China

    IEEE Chinese Guidance, Navigation and Control Conference / Institute of Electrical and Electronics Engineers / Zhong guo zi dong hua xue hui et al. | TIBKAT | 2016
    Publisher: IEEE , [Piscataway, NJ]

    Guidance, navigation and control of an unmanned helicopter for automatic cargo transportation

    Wang, Fei / Liu, Peidong / Zhao, Shiyu et al. | IEEE | 2014
    This paper presents an intelligent and robust guidance, navigation and control solution for a rotorcraft UAV to perform automatic cargo ...
    Publisher: IEEE

    Integrated design of missile guidance and control: Active disturbance rejection control method

    Ran, Maopeng / Chen, Yifen / Wang, Qing et al. | IEEE | 2014
    In this paper, we present an active disturbance rejection control (ADRC) based integrated guidance and control (IGC) law. The IGC law is ...
    Publisher: IEEE

    Integrated guidance and control with terminal angle constraint

    Han, Yang / Guo, Hongwu / Chong, Yuhai | IEEE | 2014
    Integrated guidance and control laws have the potential to improve the overall performance of missile systems by taking advantage of the ...
    Publisher: IEEE

    The application of proportional navigation in the process of UAV air combat guidance and optimization of proportional parameter

    Wang, Hui / Guan, Zuoyu / Yu, Lijun | IEEE | 2014
    navigation model is suggested for being used in the air combat Unmanned Aerial Vehicle guidance model. In addition, the value of proportional ...
    Publisher: IEEE

    Integrated guidance control with sliding mode differentiator and neural network

    Zhou, Jin / Lei, Humin / Zhang, Xu | IEEE | 2014
    missile guidance and control with sliding mode differentiator and neural network algorithm is proposed in this paper. The three dimensional target ...
    Publisher: IEEE

    Fault-tolerant guidance and control design for reentry hypersonic flight vehicles based on control-allocation approach

    Qian, Jiasong / Qi, Ruiyun / Jiang, Bin | IEEE | 2014
    In this paper, an integrated fault-tolerant guidance and control scheme is proposed for reentry hypersonic vehicles. Firstly, a predictor ...
    Publisher: IEEE

    IEEE CGNCC2014 author index

    IEEE | 2014
    Presents an index of the authors whose articles are published in the conference proceedings record. ...
    Publisher: IEEE

    Integrated navigation and pilotage systems

    Adamski, Miroslaw / Vogt, Ryszard / Cwiklak, Janusz | IEEE | 2014
    Integrated navigation and pilotage systems are mainly used in missiles, bombs and unmanned armed vehicles designed for combat purposes of ...
    Publisher: IEEE

    Adaptive integrated guidance and control with actuator failures based on backstepping and input-to-state stability

    Fei, Liao / Kaihong, Yang / Haibo, Ji | IEEE | 2014
    A fault-tolerant integrated guidance and control law is proposed based on backstepping and input-to-state stability in the presence of ...
    Publisher: IEEE

    Control method of soft landing on asteroid based on the optimal sliding-mode guidance law

    Wang, Qian-qian / Xie, Mu-jun / Li, Yuan-chun | IEEE | 2014
    Landing an asteroid safely is an important link in the deep space exploration. A kind of soft landing guidance control law about terminal ...
    Publisher: IEEE

    Observability analysis of SINS/odometer integrated navigation

    Zhang, Xiaoyue / Liu, Pengbo / Yi, Xiaojing et al. | IEEE | 2014
    An integrated navigation method of strapdown inertial navigation system(SINS) and odometer basing on Kalman filter was introduced. In the ...
    Publisher: IEEE

    Design and implementation of GPS/INS integrated navigation simulation software

    Xiu-zhen, Wu / Shao-lei, Zhou / Rui-tao, Li | IEEE | 2014
    advantages in contrast to pure inertial navigation; Based on the search model of terminal guidance radar, the hit probability calculation module of ...
    Publisher: IEEE

    Research of polarization sensor and MEMS integrated navigation system technology

    Kai, Liu / Leilei, Li / Jiabin, Chen et al. | IEEE | 2014
    size, etc. But MEMS cannot be used in initial alignment alone because of its drift and noise. Since polarization navigation sensor's errors are ...
    Publisher: IEEE

    Indoor localization, navigation and mapping for quad-rotor

    Zhou, Shaolei / Kang, Yuhang / Shi, Xianjun | IEEE | 2014
    While localizing and navigating quad-rotor, making use of the data collected by laser range-finder in the process of localization and ...
    Publisher: IEEE

    An in-motion alignment method for inertial navigation system based on unfalsified adaptive control theory

    Han, Yongqiang / Safonov, Michael G. / Chen, Jiabin | IEEE | 2014
    problem of Inertial Navigation System (SINS). The typical way of solving the problem is through filtering, yet the major factor that affects the ...
    Publisher: IEEE