A Tethered Towing Method for Space Debris Removal
A space debris and tethering technology, applied in the aerospace field, can solve the problems of system instability, affecting the success or failure of the mission, and difficult to control the attitude movement of space debris.
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[0157] In order to verify the feasibility of the method, a set of numerical simulation results are given below. The initial parameters of the tethered towed system with space debris are listed in Table 1.
[0158] Table 1 Numerical simulation parameters
[0159]
[0160]
[0161] The tethered drag system with space debris runs in a circular orbit around the earth as a whole, such as figure 1 shown. Consider two flexible sailboards installed symmetrically on the space debris, denoted as sailboards 1 and 2 respectively. The connection point between the tether and the tugboat is located at the center of mass of the tugboat. The tether is bifurcated into four sub-ropes at point B. The sub-ropes 1 and 2 are connected to the upper and lower ends of the sailboard 1, and the sub-ropes 3 and 4 are respectively connected to the sailboard. 2's lower and upper ends, such as figure 2 As shown, the elastic coefficient and viscous damping coefficient of each rope are the same. Fo...
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