device for regulating the relative positions of a group of in formation flying spacecraft through analysis of zweifrequenzsignalen

• 1. 基于事件触发的航天器编队飞行相对位置协同控制方法 [P] . 中国专利： CN109002058B . 2020.04.24
• 2. 一种通信和计算约束下航天器编队飞行相对位置控制方法 [P] . 中国专利： CN108897340B . 2020.09.04
• 3. device for regulating the relative positions of a group of in formation flying spacecraft through analysis of zweifrequenzsignalen [P] . AT460680T . 2010-03-15

  机译： zweifrequenznzsignalen分析调整编队飞行航天器相对位置的装置

• 4. Position control device (s) relative (s) by analysis of dual frequency signals to a spacecraft from a group of spacecraft formation. [P] . ES2340062T3 . 2010-05-28

  机译： 位置控制装置是通过分析来自一组航天器编队的双频信号到航天器的相对来实现的。

• 5. DEVICE CONTROL OF RELATIVE (s) position (s) by the analysis of two-frequency signals for spacecraft GROUPS OF SPACECRAFT IN FLIGHT STORY [P] . 俄罗斯专利： RU2008133983A . 2010-02-27

  机译： 通过分析飞行故事中太空飞船群的两个频率信号来控制相对位置的设备

• 1. GPS/VISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying [J] . Xiaoliang Wang, Xiaowei Shao, Deren Gong, 系统工程与电子技术（英文版） . 2011,第002期
• 2. GPSNISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying [J] . Xiaoliang Wang, Xiaowei Shao, Deren Gong, 系统工程与电子技术：英文版 . 2011,第002期
• 3. A stealthy method to determine the relative position and velocity for satellite formation flying [J] . 田继超, 崔乃刚, 姚劼, 哈尔滨工业大学学报：英文版 . 2010,第001期
• 4. A stealthy method to determine the relative position and velocity for satellite formation flying [J] . TIAN Ji-chao, CUI Nai-gang, YAO Jie, 哈尔滨工业大学学报（英文版） . 2010,第001期
• 5. USEFUL RELATIVE MOTION DESCRIPTION METHOD FOR PERTURBATIONS ANALYSIS IN SATELLITE FORMATION FLYING [J] . MENG Xin, LI Jun-feng, GAO Yun-feng 应用数学和力学（英文版） . 2005,第011期
• 6. Nonlinear suboptimal synchronized control for relative position and relative attitude tracking of spacecraft formation flying [J] . Wu Jinjie, Han Dapeng, Liu Kun, Journal of the Franklin Institute . 2015,第4期
• 7. Relative positioning of formation-flying spacecraft using single-receiver GPS carrier phase ambiguity fixing [J] . Allende-Alba Gerardo, Montenbruck Oliver, Hackel Stefan, GPS Solutions . 2018,第3期
• 8. Relative position coordinated control for spacecraft formation flying with communication delays [J] . Ran Dechao, Chen Xiaoqian, Misra Arun K., Acta astronautica . 2017,第auga期
• 9. The Key Role and Advantages of GNSS Precise Relative Positioning in Spacecraft Formation Flying Missions Design, Analysis and Operations [C] . Michelangelo Ambrosini International conference on space operations . 2018
• 10. Relative Orbit Determination For Autonomous Close Formation Flying Spacecraft. [D] . Tavvafi, Ramin. 2010
• 11. A Submillimeter-Level Relative Navigation Technology for Spacecraft Formation Flying in Highly Elliptical Orbit [O] . Xiaoliang Wang, Deren Gong, Yifei Jiang, 2020
• 12. Analysis of relative navigation architectures for formation flying spacecrafts [O] . Lefebvre de Plinval-Salgues Henry Jacques 2006

• 1. 精确测量编队飞行卫星的相对位置 [C] . 林雪 ,张育林 ,刘昆 . 中国航空学会火箭发动机委员会,中国机械工程学会复合材料委员会,中国复合材料学会教育与科普委员会2001年学术研讨会 . 2001
• 2. 编队飞行航天器相对轨道与姿态控制方法研究 [A] . 刘瑞霞 . 2019