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2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC)最新文献

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Trajectory Optimization for Target Localization and Sensor Bias Calibration with Bearing-only Information 基于方位信息的目标定位和传感器偏差标定轨迹优化
Pub Date : 2022-08-22 DOI: 10.1142/s2737480722500157
Xiwen Yang, Shaoming He, Hyo-Sang Shin, A. Tsourdos
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引用次数: 2
A nonlinear optimal control method for attitude stabilization of micro-satellites 微卫星姿态稳定的非线性最优控制方法
Pub Date : 2022-08-22 DOI: 10.1142/s2737480722500169
G. Rigatos, M. Abbaszadeh, K. Busawon, L. Dala
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引用次数: 0
Experimental Validation of an Effective Control Mechanism to Enable Flapping Wing Rotor Stable Flight 扑翼旋翼稳定飞行有效控制机制的实验验证
Pub Date : 2022-07-15 DOI: 10.1142/s2737480722500145
Ziyu Wang, Xin Dong, J. Xiang, Daochun Li, Zhan Tu
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引用次数: 0
Multi-UAV Synchronous Approaching Using Homotopy-Based Trajectory Planning 基于同伦轨迹规划的多无人机同步逼近
Pub Date : 2022-06-17 DOI: 10.1142/s2737480722500121
Weiran Yao, Yang Chen, Haoyu Tian, Chengwei Wu, Ligang Wu
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引用次数: 2
A Parallel Mapping and Planning Strategy For Micro Aerial Vehicle 微型飞行器的并行映射与规划策略
Pub Date : 2022-06-17 DOI: 10.1142/s2737480722500133
Zhuo Wang, Q. Zong, Hongming Shen, Bailing Tian, Hanchen Lu
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引用次数: 0
Magnetic Field and Radial Force Analysis of Six-phase Rotary Machine 六相旋转电机磁场及径向力分析
Pub Date : 2022-06-10 DOI: 10.1142/s273748072250011x
Z. Dong, Liang Yan, C. Gerada
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引用次数: 0
Fractional Order Darwinian Pigeon-inspired Optimization for Multi-UAV Swarm Controller 基于分数阶达尔文鸽子的多无人机群控制器优化
Pub Date : 2022-06-04 DOI: 10.1142/s2737480722500108
Bingda Tong, Chen Wei, Yuhui Shi
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引用次数: 2
Robust Event-Triggered Control of Nonlinear Systems Under a Global Sector-Bound Condition* 全局扇区约束条件下非线性系统的鲁棒事件触发控制*
Pub Date : 2022-05-07 DOI: 10.1142/s2737480722500091
Pengpeng Zhang, Tengfei Liu, Zhong-Ping Jiang
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引用次数: 0
Accelerometer Bias and Star Sensor Installation Error Joint Calibration for the SINS/CNS Integrated Navigation System Using Attitude Maneuver 基于姿态机动的SINS/CNS组合导航系统加速度计偏差与星敏感器安装误差联合标定
Pub Date : 2022-05-05 DOI: 10.1142/s2737480722500066
X. Ning, Yuqing Yang, Xiaoyu Liang, Jie Zhang
The integrated strap-down inertial navigation system/celestial navigation system (SINS/CNS) is an important autonomous navigation method with effective concealment and high precision. Both accelerometer bias and star sensor installation error are important factors that affect the performance of this navigation system, which need to be calibrated and compensated. A new accelerometer bias and star sensor installation error joint calibration method for the SINS/CNS integrated navigation system is proposed. In this newly proposed method, the installation error of star sensor is augmented to the state vector, and the star vector, nadir angle, horizontal position error and velocity error are used as measurements to calibrate the two errors mentioned above. Simulations show that both accelerometer bias and star sensor installation error can be calibrated effectively.
捷联惯导/天体导航系统(SINS/CNS)是一种重要的自主导航方法,具有有效的隐蔽性和高精度。加速度计偏差和星敏感器安装误差都是影响该导航系统性能的重要因素,需要进行标定和补偿。提出了一种新的SINS/CNS组合导航系统加速度计偏置和星敏感器安装误差联合标定方法。该方法将星敏感器的安装误差增广为状态矢量,并以星矢量、最低点角、水平位置误差和速度误差作为测量值对上述两个误差进行标定。仿真结果表明,该方法可以有效地校正加速度计偏差和星敏感器安装误差。
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引用次数: 0
Observer-based Fuzzy Sliding Mode Attitude Control for Flexible Spacecraft 基于观测器的柔性航天器模糊滑模姿态控制
Pub Date : 2022-04-18 DOI: 10.1142/s2737480722500042
Yu-Tian Xu, A. Wu
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引用次数: 0
期刊
2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC)
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