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Stable Estimation of Horizontal Velocity for Planetary Lander with Motion Constraints
被引量:
1
1
作者
Wei Shao
Shulin Sui
+1 位作者
Lin Meng
yaobin yue
《IEEE/CAA Journal of Automatica Sinica》
SCIE
EI
2015年第2期198-206,共9页
The planetary lander usually selects image feature points and tracks them from frame to frame in order to determine its own position and velocity during landing. Aiming to keep features tracking in consecutive frames,...
The planetary lander usually selects image feature points and tracks them from frame to frame in order to determine its own position and velocity during landing. Aiming to keep features tracking in consecutive frames, this paper proposes an approach of calculating the field of view (FOV) overlapping area in a 2D plane. Then the rotational and translational motion constraints of the lander can be found. If the FOVs intersects each other, the horizontal velocity of the lander is quickly estimated based on the least square method after the ill-conditioned matrices are eliminated previously. The Monte Carlo simulation results show that the proposed approach is not only able to recover the ego-motion of planetary lander, but also improves the stabilization performance. The relationship of the estimation error, running time and number of points is shown in the simulation results as well. © 2014 Chinese Association of Automation.
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关键词
Intelligent
systems
LANDING
Least
squares
approximations
Monte
Carlo
methods
VELOCITY
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职称材料
题名
Stable Estimation of Horizontal Velocity for Planetary Lander with Motion Constraints
被引量:
1
1
作者
Wei Shao
Shulin Sui
Lin Meng
yaobin yue
机构
College of Automation&Electronic Engineering
School of Mathematics&Physics
出处
《IEEE/CAA Journal of Automatica Sinica》
SCIE
EI
2015年第2期198-206,共9页
基金
supported by National Basic Research Program of China(973 Program)(2012CB720000)
National Natural Science Foundation of China(61104187)
Promotive Research Fund for Excellent Young and Middle-aged Scientists of Shandong Province(BS2012NY003)
文摘
The planetary lander usually selects image feature points and tracks them from frame to frame in order to determine its own position and velocity during landing. Aiming to keep features tracking in consecutive frames, this paper proposes an approach of calculating the field of view (FOV) overlapping area in a 2D plane. Then the rotational and translational motion constraints of the lander can be found. If the FOVs intersects each other, the horizontal velocity of the lander is quickly estimated based on the least square method after the ill-conditioned matrices are eliminated previously. The Monte Carlo simulation results show that the proposed approach is not only able to recover the ego-motion of planetary lander, but also improves the stabilization performance. The relationship of the estimation error, running time and number of points is shown in the simulation results as well. © 2014 Chinese Association of Automation.
关键词
Intelligent
systems
LANDING
Least
squares
approximations
Monte
Carlo
methods
VELOCITY
Keywords
Planetary landing
feature tracking
overlapping area
horizontal velocity estimation
ill-conditioned matrices
field of view(FOV)
分类号
V448.2 [航空宇航科学与技术—飞行器设计]
V525 [航空宇航科学与技术—人机与环境工程]
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1
Stable Estimation of Horizontal Velocity for Planetary Lander with Motion Constraints
Wei Shao
Shulin Sui
Lin Meng
yaobin yue
《IEEE/CAA Journal of Automatica Sinica》
SCIE
EI
2015
1
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