| [1] |
WANG Yue-Jiao, MA Zhong, YANG Yi-Dai, WANG Zhu-Ping, TANG Lei.
Satellite attitude control method based on deep reinforcement learning
[J]. , 2019, 39(4): 36-.
|
| [2] |
LIN Jia-Wei, WANG Ping.
In orbit Estimation of Satellite inertial matrix using STLS
[J]. , 2010, 30(6): 31-38.
|
| [3] |
Wang Zhisheng~1 Zhen Ziyang~1 Fan Dapeng~2 (1 College of Automation Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016) (2 College of Mechatronics Engineering and Automation, National University of Defense Technology,Changsha 410073).
Design of Federated Filtering Based Satellite Attitude Determination System
[J]. , 2009, 29(03): 1-9.
|
| [4] |
Chen Xueqin Geng Yunhai Wang Feng Zhang Yingchun(Research Center of Satellite Technology,Harbin Institute of Technology,Harbin 150080).
Satellite Attitude Fault-tolerant Control Based on Robust Adaptive Inverse Optimal Control
[J]. , 2008, 28(02): 35-41.
|
| [5] |
Li Yuan1 Wu Hongyue2 Wu Jie3(1 China Academy of Space Technology,Beijing 100094)(2 China Ship Research and Development Academy,Beijing 100085)(3 Beijing Changcheng Institute of Metrology and Measurement,Beijing 100095).
Genetic Algorithm PID Self-tuning based on the Satellite Attitude Control
[J]. , 2007, 27(04): 66-71.
|
| [6] |
Wang Yongjun Qin Yongyuan Yang Bo(Department of Automatic Control North Westem Polytechnical Univercity,Xi′an 710072).
Comparison of Quaternion and Rodrigues Parameters on Attitude Algorithm of Secondary Planet
[J]. , 2007, 27(03): 18-23.
|
| [7] |
Liu Rui Wang Ping Lü Zhenduo(Beijing Institute of Control Engineering,Beijing 100080).
Effects of Spacecraft Movable Accessory on the Attitude of Meteorological Satellite
[J]. , 2005, 25(06): 1-7.
|
| [8] |
Cai Xiaodong Ye Peijian(China Academy of Space Technology,Beijing 100094).
Research on Satellite Attitude Sensor Applying Remote Sensing Image Information
[J]. , 2005, 25(06): 8-13.
|
| [9] |
Zhang Honghua Li Kang Zhao Yu (Beijing Institute of Control Engineering, Beijing 100080).
Fast Maneuver Control of Flexible Satellite System
[J]. , 2005, 25(01): -.
|
| [10] |
Gu Dongqing Wang Yan Zhou Wenjun Qin Yongyuan(Northwestern Polytechnical University, Xi'an 710072).
Federated Filter Design for Multi-sensors Satellite Attitude Determination
[J]. , 2004, 24(03): -.
|
| [11] |
Lin Yurong Deng Zhenglong(Harbin Institute of Technology, Harbin 150001).
Research on Second-Order Nonlinear Filter Technology for Processing Satellite Attitude Measurement Information
[J]. , 2003, 23(03): -.
|
| [12] |
Li Taiyu Zhang Yulin (Inst.of Aerospace and Material Engineering,National Univ. of Defense Technology,Changsha 410073).
A New Method of Momentum Unloading Utilizing Geomagnetic Field
[J]. , 2001, 21(06): -.
|
| [13] |
Sun Baoxiang Li Mingtao Wang Dongsheng Gao Yijun Hua GengxinLiu Chengxi Wang Changlong Jian Ming Wang Yuanxi Bai Zhiying(Beijing Institute of Control Engineering,Beijing 100080).
A REALTIME TELEMETRY AND ATTITUDE DETERMINATION SYSTEM BASED ON MULTILEVEL FAULT-TOLERANT
[J]. , 1998, 18(03): -.
|
| [14] |
Li Jie(Beijing Institute of Control Engineering,Beijing 100080)).
PERFORMANCE COMPARISON OF TWO MOUNTING CONFIGURATIONS OF INFRARED EARTH SENSORS
[J]. , 1997, 17(06): -.
|
| [15] |
Lu Mingyu (Tsinghua University, Beijing 100084)Yi Kui; Yang Junfa; Deng Ruzhen (Beijing Institute of Control Engineering, Beijing 100080).
DEVELOPMENT OF A REAL-TIME SIGNAL SOURCE FOR INFRARED EARTH SENSOR
[J]. , 1996, 16(03): -.
|
