1–20 von 447 Ergebnissen
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    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
    Verlag: IEEE , [Piscataway, NJ]

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

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

    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
    Verlag: IEEE , Piscataway, NJ

    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
    Verlag: 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
    Verlag: IEEE , Piscataway, NJ

    Fault diagnosis and fault-tolerant predictive control for Hypersonic Vehicle (IEEE CGNCC)

    Yizhen Meng, / Bin Jiang, / Ruiyun Qi, et al. | IEEE | 2016
    also be sensitive to disturbances and faults, which results in a big challenge for fault-tolerant control. Therefore, a fault-tolerant control ...
    Verlag: IEEE

    The attitude decoupling control of the flying wing UAV (IEEE CGNCC)

    Jiguang Li, / Xin Chen, / Zhen Li, | IEEE | 2016
    method is put forward in the thesis. And the results of the emulation show that the attitude decoupling control of the flying wing UAV, based on ...
    Verlag: IEEE

    An improved model aided navigation method with online dynamics parameters estimation for multirotor UAV (IEEE CGNCC)

    Wenjing Chen, / Jizhou Lai, / Min Liu, et al. | IEEE | 2016
    ADM aided navigation is presented. And the feasibility of the method is verified through observability analysis. Simulation results show that ...
    Verlag: IEEE

    A GPS/INS navigation strategy of dealing with extreme cases by cooperating radar (IEEE CGNCC)

    Zhi Liu, / Huabao Long, / Jie He, et al. | IEEE | 2016
    This paper designs a strategy that monitors the system anomaly and uses radar's information to replace the GPS to complete the navigation ...
    Verlag: IEEE

    Modeling and simulation for piston engine towards flight simulator(IEEE CGNCC)

    Yong-kang Jiao, / Kun-hu Kou, / Yong Chen, | IEEE | 2016
    UAV piston engine was made up by adopting the method of combination mechanism modeling and experimental modeling, while the simulation of the ...
    Verlag: IEEE

    The application of L1 adaptation control theory for Flying-wing UAV (IEEE CGNCC)

    Xiaowei Zhang, / Chuntao Li, / Jiangling Fu, | IEEE | 2016
    Regulator(RSLQR) and L1 adaptive control method. The controlled variable is chosen as C*, a combination of longitudinal acceleration and ...
    Verlag: IEEE

    Study on the measuring device and method of sky polarization information(IEEE CGNCC)

    Gao Chi, / Zhang Heng, / Zhang Rongtao, | IEEE | 2016
    measurement method of the sky polarization information. The experiments show that the device and method can effectively improve the measurement ...
    Verlag: IEEE

    Adaptive dynamic surface control of VCM drived pointing mirror with parameter uncertainties (IEEE CGNCC)

    Chen, Zi-Yin / Lin, Zhe / Kang, Jian-Bing et al. | IEEE | 2016
    the mathematical model of the VCM, the design procedure is divided into three parts, namely the position loop, angular velocity loop and the ...
    Verlag: IEEE

    Fault diagnosis of actuator of Flight Control System based on analytic model (IEEE CGNCC)

    Dong Cao, / Jiangling Fu, / Yong Li, | IEEE | 2016
    Actuator plays an important role in the Flight Control System of UAV (Unmanned Aerial Vehicle), so it is necessary to diagnose the fault in ...
    Verlag: IEEE

    Overview of the orbit determination for CE-2 extended mission (IEEE CGNCC)

    Jianfeng, Cao / Songjie, Hu / Lei, Liu et al. | IEEE | 2014
    Chang'E-2(CE-2) extended mission started from June 2011, the maximum distance between CE-2 and the Earth is about 1,700,000 km. In this ...
    Verlag: IEEE

    Remaining Useful Life prediction for the momentum wheel considering work condition switching (IEEE CGNCC)

    Liang Jiang, / Yuehua Cheng, / Tianshe Yang, et al. | IEEE | 2016
    Given the requirements that spacecraft have long life and high reliability, the Remaining Useful Life (RTJL) prediction of a key unit! such ...
    Verlag: IEEE

    A comparison of several proposed reliability analysis methods combining Kriging and Monte Carlo Simulation (IEEE CGNCC)

    Zigan Zhao, / Zhengming Wang, / Xiaojun Duan, | IEEE | 2016
    costs and ensure the accuracy at the same time. This paper makes comparison of EGRA, AK-MCS, IBS criterion 2 and its deformation. The results ...
    Verlag: IEEE

    The guidance control system design of a miniature guided ammunition

    An, Xiao-Qian / Fan, Jun-Fang | IEEE | 2016
    autopilot can realize fast tracking in the guidance phase. This research will perform as theoretical basis for the guidance control system ...
    Verlag: IEEE

    A Nonlinear Impact-Time-Control Guidance law for salvo attack

    Qiuhui Yang, / Shaoke Qian, / Lina Geng, et al. | IEEE | 2016
    closed form expression for the guidance command is derived by introducing an indirect variable, and the performance index of a pseudo-control ...
    Verlag: IEEE

    Terminal guidance and control for kinetic kill vehicle adopting side window detection

    Huang, Jingshuai / Zhang, Hongbo / Li, Guanghua et al. | IEEE | 2016
    the condition that constraints of side window scope are satisfied. In this paper, a method of terminal guidance and control applied to kinetic ...
    Verlag: IEEE