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Mechatronic Design, Dynamic Modeling and Results of a Satellite Flight Simulator for Experimental Validation of Satellite Attitude Determination and Control Schemes in 3-Axis

机译：卫星飞行模拟器的机电一体化设计，动态建模和结果，用于三轴卫星姿态确定和控制方案的实验验证

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M.A. Mendoza-Bárcenas; E. Vicente-Vivas; H. Rodríguez-Cortés;
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年度 2014
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1. Mechatronic Design, Dynamic Modeling and Results of a Satellite Flight Simulator for Experimental Validation of Satellite Attitude Determination and Control Schemes in 3-Axis [J] . Mendoza-Bárcenas M. A., Vicente-Vivas E., Rodríguez-Cortés H. Journal of Applied Research and Technology . 2014,第3期

机译：卫星飞行模拟器的机电设计，动态建模和结果，用于三轴卫星姿态确定和控制方案的实验验证
2. Development and experimental validation of a multi-algorithmic hybrid attitude determination and control system for a small satellite [J] . Lee Dae Young, Park Hyeongjun, Romano Marcello, Aerospace science and technology . 2018,第JULa期

机译：小型卫星多算法混合姿态确定与控制系统的开发与实验验证
3. Experimental study on the dynamics and control of a space robot with experimental free-floating robot satellite (EFFORTS) simulators [J] . KAZUYA YOSHIDA Advanced Robotics . 1995,第6期

机译：带有实验自由浮动机器人卫星（EFFORTS）模拟器的空间机器人动力学和控制的实验研究
4. Study on the Determination of Attitudes and Orbits of Micro-satellites only by 3-axis Magnetometer [C] . MyongChol Jang International Conference on Aeronautical Materials and Aerospace Engineering . 2019

机译：仅通过3轴磁力计确定微卫星态度和轨道的研究
5. Design of an adaptive balancing scheme for the Small Satellite Attitude Control Simulator (SSACS). [D] . Olsen, Tanya Ann. 1994

机译：小卫星姿态控制模拟器（SSACS）的自适应平衡方案设计。
6. QMRPF-UKF Master-Slave Filtering for the Attitude Determination of Micro-Nano Satellites Using Gyro and Magnetometer [O] . Peiling Cui, Huijuan Zhang 2010

机译：使用陀螺仪和磁力计确定微纳卫星姿态的QMRPF-UKF主从滤波
7. Mechatronic Design, Dynamic Modeling and Results of a Satellite Flight Simulator for Experimental Validation of Satellite Attitude Determination and Control Schemes in 3-Axis [O] . Mendoza-Bárcenas M.A., Vicente-Vivas E., Rodríguez-Cortés H. 2014

机译：卫星飞行模拟器的机电设计，动态建模和结果，用于三轴卫星姿态确定和控制方案的实验验证
8. Attitude Control and Orbital Dynamics Challenges of Removing the First 3-Axis Stabilized Tracking and Data Relay Satellite from the Geosynchronous ARC [R] . Benet, C. A., Hofman, H., Williams, T. E., 2011

机译：从地球同步aRC中移除第一个3轴稳定跟踪和数据中继卫星的姿态控制和轨道动力学挑战

Mechatronic Design, Dynamic Modeling and Results of a Satellite Flight Simulator for Experimental Validation of Satellite Attitude Determination and Control Schemes in 3-Axis

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