METHOD AND SYSTEM FOR ESTIMATING THE DIRECTION OF A TRANSFER SATELLITE SATELLITE FROM AN INITIAL ORBIT TO A MISSION ORBIT

• 1. 用于估计在从初始轨道到任务轨道的转移阶段中卫星的方向的方法和系统 [P] . 中国专利： CN109791189B . 2020.08.11
• 2. 用于估计在从初始轨道到任务轨道的转移阶段中卫星的方向的方法和系统 [P] . 中国专利： CN109791189A . 2019-05-21
• 3. METHOD AND SYSTEM FOR ESTIMATING THE DIRECTION OF A SATELLITE IN THE TRANSFER PHASE FROM AN INITIAL ORBIT TO A MISSION ORBIT [P] . EP3491408B1 . 2021-07-14

  机译： 从初始轨道到任务轨道估计转移阶段中卫星方向的方法和系统

• 4. METHOD AND SYSTEM FOR ESTIMATING THE DIRECTION OF A SATELLITE IN THE TRANSFER PHASE FROM AN INITIAL ORBIT TO A MISSION ORBIT [P] . 美国专利： US2019217974A1 . 2019-07-18

  机译： 估算从初始轨道到发射轨道的转移阶段中卫星方向的方法和系统

• 5. METHOD AND SYSTEM FOR ESTIMATING THE DIRECTION OF A SATELLITE IN THE TRANSFER PHASE FROM AN INITIAL ORBIT TO A MISSION ORBIT [P] . 欧洲知识产权局专利： EP3491408A2 . 2019-06-05

  机译： 估算从初始轨道到发射轨道的转移阶段中卫星方向的方法和系统

• 1. Selection of the best initial orbital elements of satellite based on fuzzy integration evaluation method [J] . Yang Yongan, Zhang Hongwei, Feng Zuren, 系统工程与电子技术（英文版） . 2006,第003期
• 2. Multi-objective evolutionary optimization for geostationary orbit satellite mission planning [J] . Jiting Li, Sheng Zhang, Xiaolu Liu, 系统工程与电子技术（英文版） . 2017,第005期
• 3. Shift control method for the local time at descending node based on sun-synchronous orbit satellite [J] . Yang Yongan, Feng Zuren, Sun Linyan, 系统工程与电子技术（英文版） . 2009,第001期
• 4. Single-Impulse Transfers from Orbits of Artificial Satellites to Orbits around Lx or L2 Libration Points [J] . B. B. Kreisman Cosmic research . 2011,第4期
• 5. PARAMETERS OPTIMIZATION OF A LOW- ORBIT SMALL SATELLITES BATCHING USING THE RANGE-DIFFERENCE METHOD IN ORDER TO ESTIMATE RADIO SOURCES COORDINATES [J] . M.V. Mironov, V.A. Gromov, E.P. Voroshilin, Telecommunications and Radio Engineering . 2011,第6期
• 6. Homogeneous and Heterogeneous Observational Data Weighting Method of Combined Orbit Determination of Near-earth Satellites of Bi-satellite Positioning System and its Applications [J] . De-Yong Zhao, Xiao-Gong Pan, Jiong-Qi Wang, Chinese Astronomy and Astrophysics . 2008,第3期
• 7. A Comparative Thermal Study of a GEO Satellite for Geostationary Transfer Orbit and Mission Orbit [C] . Muhammed Uğur Carfi, Bilal Burak Doğan International Conference on Recent Advances in Space Technologies . 2019
• 8. Initial thermal design of microchannel heat sink for low-orbit micro-satellites. [D] . Heresztyn, Amaury Jean Henri. 2004
• 9. A Robust Method to Detect BeiDou Navigation Satellite System Orbit Maneuvering/Anomalies and Its Applications to Precise Orbit Determination [O] . Fei Ye, Yunbin Yuan, Bingfeng Tan, 2017
• 10. Two-Site Optical Observation and Initial Orbit Determination for Geostationary Earth Orbit Satellites [O] . Jin Choi, Young-Jun Choi, Hong-Suh Yim, 2010

• 1. FY-3E:The First Operational Meteorological Satellite Mission in an Early Morning Orbit [J] . Peng ZHANG ,Xiuqing HU ,Qifeng LU . 大气科学进展:英文版 . 2022,第1期
• 2. The Injection Velocity and Apogee Simulation for Transfer Elliptical Satellite Orbits [J] . Shkelzen Cakaj ,Bexhet Kamo ,Vladi Kolici . 通讯、网络与系统学国际期刊（英文） . 2012,第3期
• 3. 基于测距系统的中继卫星轨道机动检测方法研究 [C] . 郭翔宇 ,张俊丽 . 第六届中国卫星导航与位置服务年会 . 2017
• 4. 共线平动点附近二体绳系卫星系统轨道保持控制方法研究 [A] . 刘刚 . 2015