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中文核心期刊

Theme Articles on Aerospace Dynamics and Control

DYNAMIC SIMULATION ANALYSIS OF CAPTURE AND BUFFER SYSTEM BASED ON CLAW-TYPE DOCKING MECHANISM
Shen Tao, Zhang Chongfeng, Wang Weijun, Feng Wenbo, Qiu Huayong
2020, 52(6): 1590-1598. 2020, 52(6): 1590-1598.  doi: 10.6052/0459-1879-20-108
SPACECRAFT EVASION STRATEGY USING ACTIVE MANEUVERS BASED ON MANEUVERING-TARGET ACCELERATION ESTIMATION
Li Haohao, Zhang Jin, Luo Yazhong
2020, 52(6): 1560-1568. 2020, 52(6): 1560-1568.  doi: 10.6052/0459-1879-20-113
A COLLISION-AVOIDANCE CONTROL ALGORITHM FOR SPACECRAFT PROXIMITY OPERATIONS BASED ON IMPROVED ARTIFICIAL POTENTIAL FUNCTION
Xu D, an
2020, 52(6): 1581-1589. 2020, 52(6): 1581-1589.  doi: 10.6052/0459-1879-20-112
DYNAMICS AND CONTROL OF RIGID-FLEXIBLE COUPLING FLEXIBLE SPACECRAFT WITH JOINT CLEARANCE
Sun Jie, Sun Jun, Liu Fucheng, Zhu Dongfang, Huang Jing
2020, 52(6): 1569-1580. 2020, 52(6): 1569-1580.  doi: 10.6052/0459-1879-20-109
DYNAMIC MODELING AND STABILITY CONTROL OF FOLDING WING AIRCRAFT
Song Huixin, Jin Lei
2020, 52(6): 1548-1559. 2020, 52(6): 1548-1559.  doi: 10.6052/0459-1879-20-115
ATTITUDE CONTROL TECHNOLOGY FOR MASS MOMENT NANO-SATELLITE IN LOW EARTH ORBIT
Hu Yu, , Lu Zhengliang
2020, 52(6): 1599-1609. 2020, 52(6): 1599-1609.  doi: 10.6052/0459-1879-20-116
航天动力学与控制专题序
2020, 52(6): 1547-1547. 2020, 52(6): 1547-1547.  doi: 10.6052/0459-1879-20-377
FAST OPTIMIZATION METHOD OF REENTRY TRAJECTORY CONSIDERING AERODYNAMIC PARAMETER PERTURBATION
Yang Ben, Lei Jianchang, Wang Yuhang
2020, 52(6): 1610-1620. 2020, 52(6): 1610-1620.  doi: 10.6052/0459-1879-20-117
AN ALGORITHM FOR SOLVING SPACECRAFT REACHABLE DOMAIN WITH SINGLE-IMPULSE MANEUVERING
Du Xiangnan, Yang Zhen
2020, 52(6): 1621-1631. 2020, 52(6): 1621-1631.  doi: 10.6052/0459-1879-20-111