[1] |
CHENG Haibin, LU Hao, XU Jianyun.
A polar navigation algorithm of strapdown inertial navigation system under frozen geography frame
[J]. Chinese Space Science and Technology, 2020, 40(2): 35-.
|
[2] |
HE Cheng-Long, YU Bao-Guo.
Ranging Error Caused by MAI in Terrestrial Pseudolites System and its Correction Method
[J]. Chinese Space Science and Technology, 2015, 35(5): 8-14.
|
[3] |
DUAN Guang-Ren, ZHANG Ze, SUN Yong.
Algorithm for Coning Error Compensation Based on Angular Velocity
[J]. Chinese Space Science and Technology, 2012, 32(1): 15-20.
|
[4] |
Liu Ruihua Zhang Fan (Institute of CNS/ATM,Civil Aviation University of China,Tianjin 300300).
Passive Location Method of Beidou Geostationary Satellites Positioning System Aided by Pseudolites
[J]. Chinese Space Science and Technology, 2010, 30(04): 52-57.
|
[5] |
Wang Wei1 Liu Zongyu2(1 School of Instrument Science & Opt-electronics Engineering,Beihang University,Beijing 100083) (2 Beijing Institute of Control Engineering,Beijing 100083).
Augmented Beidou Satellite System by Airborne Pseudolites
[J]. Chinese Space Science and Technology, 2010, 30(03): 19-24.
|
[6] |
Liu Tong Li Zhibin (Beijing Institute of Control Engineering,Beijing 100080).
Application of SINS/GPS/Landmark Integrated Navigation in Stratospheric Airship
[J]. Chinese Space Science and Technology, 2008, 28(03): 29-36+44.
|
[7] |
Pan Xiaogang Zhou Haiyin(Department of Mathematic and System Science,National University of Defense Technology,Changsha 410073).
Research on Method of Spacecraft Orbit Determination Based on Penalized Least Squares Estimation
[J]. Chinese Space Science and Technology, 2008, 28(02): 15-20+50.
|
[8] |
Yang Bo1 Qin Yongyuan2 Chai Yan3 Peng Huihuang4(1 The Second Artillery Engineering College,Xi'an 710025)(2 College of Automation,Northwestern Polytechnical University,Xi'an 710072)(3 School of Materials,Northwestern Polytechnical University,Xi'an 710072)(4 The Military Deputy Office of the Second Artillery in Factory of Hong Yang,Xiaogan 432100).
Research and Simulation on Precise SINS/CCD/GPS Integrated Navigation System
[J]. Chinese Space Science and Technology, 2008, 28(02): 42-50.
|
[9] |
Du Yaling Liu Jianye Xiong Zhi(Navigation Research Center,Nanjing University of Aeronautics & Astronautics,Nanjing 210016)Jiang Yong(Unmanned Aerial Vehicles Research Department,Nanjing University of Aeronautics & Astronautics,Nanjing 210016).
The Attitude Integrated Algorithm in Complete Integrated GPS/SINS Navigation System
[J]. Chinese Space Science and Technology, 2006, 26(01): 53-58.
|
[10] |
Wang Peng Zhang Yingchun Qiang Wenyi Zhang Ronglin(Research Center of Satellite Technology,Harbin Institute of Technology,Harbin 150080).
Study of the Strap-down Inertial Navigation System/Star Sensor Integrated Navigation System Algorithms
[J]. Chinese Space Science and Technology, 2005, 25(06): 19-25+29.
|
[11] |
Wang Wei Liu Zongyu Xie Rongrong (Automation School of Northwestern Polytechnical University, Xi'an 710072).
Study on Pseudolite-augmented “Bei dou” Double-star Positioning System and Algorithm
[J]. Chinese Space Science and Technology, 2005, 25(03): 66-71.
|
[12] |
Lai Jizhou Liu Jianye Lin Xueyuan Xiong Zhi Zeng Qinghua (Navigation Research Center, Nanjing University of Aeronautics and Astronautics, Nanjing 210016).
Realization and Research of Low Order Kalman Filter for the Low-Cost SIAHRS
[J]. Chinese Space Science and Technology, 2004, 24(01): -.
|
[13] |
Liu Ruihua (College of ATM, Civil Aviation University of China, Tianjin 300300).
The Minimal Parameter Solution for the Quaternion Differential Equation
[J]. Chinese Space Science and Technology, 2003, 23(06): -.
|
[14] |
Xiong Zhi Liu Jianye Lin Xueyuan (Navigation Research Center, Nanjing University of Aeronautics & Astronautics Nanjing 210016)$$$$.
Research of INS/SAR Integrated Navigation System Aided by Height
[J]. Chinese Space Science and Technology, 2003, 23(04): -.
|
[15] |
Lin Xueyuan Liu Jianye Wang Shuhua (Navigation Research Center, Nanjing University of Aeronautics and Astronautics, Nanjing 210016)$$$$.
The Study on Double-Star Position/SINS Integration Navigation System
[J]. Chinese Space Science and Technology, 2003, 23(02): -.
|