Result found by MTS

Citation Author(s):
Zhong
Zhang
Submitted by:
Zhong Zhang
Last updated:
Sun, 05/23/2021 - 23:50
DOI:
10.21227/yxkh-6r96
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License:
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Abstract 

This is the result found by multi-tree-search.</p>

Instructions: 

This is the result found by multi-tree-search.
(1) Column 1 is the line number.
(2) Column 2 is the satellite: "1" for optical satellite and "2" for infrared satellite.
(3) Column 3 is the action: "0" for setting initial orbital parameters, "1" for implementing impulse, "2" for observing targets, and "3" for starting to transmit with relay satellites.
(4) Column 4 is the action time (s), which represents the cumulative seconds from the initial time (1 January 2020 00:00:00).
(5) Columns 5~7 and Columns 8~10 are the position components (km) and velocity components (km/s) at the time shown in the same line of Column 4, respectively, and they are expressed in the ECI frame. If an impulse is performed, Columns 8~10 provide the velocity components
after the impulse.
(6) Columns 11~13 are the impulse vector (km/s) in the ECI frame. If the corresponding action flag (Column 3) is not "1", fill "0".
(7) Column 14 is the remaining mass (kg) of the satellite. If an impulse is performed, fill the mass after the impulse.
(8) Column 15 is the number of the target points. 1~200 denote the stationary targets, and 1001~1004 denote the relay satellite number. Fill "0" if the action flag is "1"; fill the target number if the action flag is "2"; fill the relay satellite number if the action flag is "3".