[1] |
LYU Nan, GUO Jianxin, XIAO Shuai, LIN Bo, ZHONG Xiaoqing, ZHOU Zhicheng.
A Review on Development of Control Techniques for DFH-Series Communication Satellites
[J]. Aerospace Contrd and Application, 2024, 50(5): 1-16.
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[2] |
LI Wei, LIANG Xingang, LI Fei, MA Xue.
Design and Application of Separate Propulsion System for Full Electric Propulsion Satellite
[J]. Aerospace Contrd and Application, 2024, 50(5): 55-61.
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[3] |
GUAN Tao, LI Bin, WU Yunli.
Finite Time Spacecraft Attitude Reorientation Control Under Pointing Constrains
[J]. Aerospace Contrd and Application, 2024, 50(3): 52-59.
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[4] |
HUANG Lirong, ZENG Zhezhao, ZENG Peng.
Auto Coupling PD Attitude Control Method for Flexible Spacecraft
[J]. Aerospace Contrd and Application, 2024, 50(1): 75-83.
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[5] |
WU Xiaoming , JU Meiqi, LIN Jiawei, WANG Mengfei, SUN Tianyi, GAO Xinyu.
Application of Virtual Test Technology in Satellite Development
[J]. Aerospace Contrd and Application, 2023, 49(2): 83-89.
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[6] |
LI Bingke, YU Yanbo, WANG Shuquan, TAN Yonghua, YUE Wenlong .
Spacecraft Power Optimal Attitude Control Using Control Momentum Gyroscopes
[J]. Aerospace Contrd and Application, 2023, 49(1): 30-39.
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[7] |
MIAO Haibin, LIU Hongjin, LYU Quanxiu, SHAO Lizhen.
Attitude Control of Micro Nano Satellite Group Based on Multi Objective Optimization
[J]. Aerospace Contrd and Application, 2023, 49(1): 21-29.
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[8] |
LIN Bo, CHANG JianSong, LIU Xinyan.
An Attitude Control Method Based on Pseudo Rate Modulator for Eliminating Self Excited Oscillation
[J]. Aerospace Contrd and Application, 2022, 48(6): 40-45.
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[9] |
ZHOU Yiwen, ZHONG Kewei, ZHANG Wanchao, JIN Yihuan, JIANG Huchao.
Adaptive attitude control of super twisting sliding mode for near space vehicle
[J]. Aerospace Contrd and Application, 2022, 48(1): 9-15.
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[10] |
XIE Jun, WANG Ping.
Development and Contributions of Beidou Navigation Satellite Attitude and Orbit Control Technologies
[J]. Aerospace Contrd and Application, 2021, 47(5): 1-8.
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[11] |
WANG Hongru, LIU Yunping, MA Jinhu, YAN Le.
Series Parallel PID Control of Underwater Vehicles Based on Singular Perturbation Method
[J]. Aerospace Contrd and Application, 2021, 47(3): 40-48.
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[12] |
WANG Yang, GONG Wei, ZHANG Jiangwei, YU Qi, ZHU Bofan.
Interval Parameterization Method for Spacecraft Attitude Control
[J]. Aerospace Contrd and Application, 2020, 46(5): 59-64.
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[13] |
CUI Yufei, DENG Sier, DENG Kaiwen, ZHANG Wenhu, CUI Yongcun.
Friction Torque Characteristics of Control Moment Gyros Bearing Unit
[J]. Aerospace Contrd and Application, 2020, 46(5): 73-80.
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[14] |
Design of B Data Bus Protocol Based on ECSS for Spacecraft Attitude and Orbit Control System.
Design of 1553B Data Bus Protocol Based on ECSS for Spacecraft Attitude and Orbit Control System
[J]. Aerospace Contrd and Application, 2020, 46(2): 41-48.
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[15] |
Robust PD+ Controller with Fast Convergence Rate for Satellite Attitude Tracking a Dynamic Target.
Robust PD+ Controller with Fast Convergence Rate for Satellite Attitude Tracking a Dynamic Target
[J]. Aerospace Contrd and Application, 2020, 46(2): 16-21.
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