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浏览/检索结果: 共6条，第1-6条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Initial attitude estimation and installation errors calibration of the IMU for plane by SINS/CNS integration 期刊论文 Lecture Notes in Electrical Engineering, 2018, 卷号: 458, 页码: 123-130 作者:  Yuan, W.;  Gui, M.;  Ning, X. 收藏  |  浏览/下载：10/0  |  提交时间：2019/12/30 Air navigation  Calibration  Gyroscopes  Inertial navigation systems  Navigation systems  Units of measurement  Attitude estimation  Autonomous navigation  Celestial measurements  Horizontal velocity  Inertial measurement unit  Installation error  Integrated navigation  Strap-down inertial navigation systems  Errors   Classification of Methods in the SINS/CNS Integration Navigation System 期刊论文 IEEE ACCESS, 2018, 卷号: 6, 页码: 3149-3158 作者:  Yang, Yanqiang;  Zhang, Chunxi;  Lu, Jiazhen;  Zhang, Hao 收藏  |  浏览/下载：7/0  |  提交时间：2019/12/30 Strap-down inertial navigation system (SINS)  celestial navigation system (CNS)  attitude observation  star vector observation   Initial Attitude Estimation and Installation Errors Calibration of the IMU for Plane by SINS/CNS Integration 会议论文 PROCEEDINGS OF 2017 CHINESE INTELLIGENT AUTOMATION CONFERENCE, 2018-01-01 作者:  Yuan, Weiping;  Gui, Mingzhen;  Ning, Xiaolin 收藏  |  浏览/下载：7/0  |  提交时间：2019/12/30 In-Flight Calibration of Gyros and Star Sensor With Observability Analysis for SINS/CNS Integration 期刊论文 IEEE SENSORS JOURNAL, 2017, 卷号: 17, 页码: 7131-7142 作者:  Yang, Yanqiang;  Zhang, Chunxi;  Lu, Jiazhen;  Zhang, Hao 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/30 SINS/CNS integration  observability degree  gyro all-parameter errors calibration  star sensor installation errors   Local Observability Analysis of Star Sensor Installation Errors in a SINS/CNS Integration System for Near-Earth Flight Vehicles 期刊论文 SENSORS, 2017, 卷号: 17 作者:  Yang, Yanqiang;  Zhang, Chunxi;  Lu, Jiazhen 收藏  |  浏览/下载：1/0  |  提交时间：2019/12/30 star sensor installation errors  local observability analysis  Kalman Filtering  near-earth flight vehicles   A reliable multi-sensor navigation system for an unmanned aerial vehicle realized through integration of SINS with GPS, CNS and doppler radar 会议论文 5th International Conference on Mechanical and Electrical Technology, ICMET 2013, Chengdu, China, 2013-07-20 作者:  Ushaq, Muhammad;  Cheng, Fang Jian 收藏  |  浏览/下载：5/0  |  提交时间：2020/01/06